U.S. patent application number 10/088476 was filed with the patent office on 2002-11-21 for exhaust gas purification device.
Invention is credited to Asanuma, Takamitsu, Hirota, Shinya, Itoh, Kazuhiro, Kimura, Koichi, Nakatani, Koichiro, Tanaka, Toshiaka.
Application Number | 20020170287 10/088476 |
Document ID | / |
Family ID | 27481483 |
Filed Date | 2002-11-21 |
United States Patent
Application |
20020170287 |
Kind Code |
A1 |
Hirota, Shinya ; et
al. |
November 21, 2002 |
Exhaust gas purification device
Abstract
An exhaust gas purification apparatus, for an engine (1) having
a combustion chamber (5), comprising an exhaust passage (10), a
particulate filter arranged in the exhaust passage for removing
particulate in exhaust gas exhausted from the combustion chamber by
oxidation, and a device (30) for controlling the characteristics of
the exhaust gas flowing into the particulate filter, wherein, when
the judging means judges that the particulate filter will the
characteristics of the exhaust gas flowing into the particulate
filter to prevent the particulate filter from being deteriorated by
heat.
Inventors: |
Hirota, Shinya;
(Shizuoka-ken, JP) ; Tanaka, Toshiaka;
(Shizuoka-ken, JP) ; Itoh, Kazuhiro;
(Shizuoka-ken, JP) ; Asanuma, Takamitsu;
(Shizuoka-ken, JP) ; Nakatani, Koichiro;
(Shizuoka-ken, JP) ; Kimura, Koichi;
(Shizuoka-ken, JP) |
Correspondence
Address: |
Oliff & Berride
P O Box 19928
Alexandria
VA
22320
US
|
Family ID: |
27481483 |
Appl. No.: |
10/088476 |
Filed: |
March 20, 2002 |
PCT Filed: |
July 23, 2001 |
PCT NO: |
PCT/JP01/06350 |
Current U.S.
Class: |
60/277 ; 60/295;
60/297; 60/311 |
Current CPC
Class: |
F01N 2900/0422 20130101;
F01N 3/0885 20130101; F01N 3/0821 20130101; F02D 2200/0818
20130101; F02M 26/10 20160201; F02D 41/0245 20130101; F01N 3/032
20130101; F02D 41/187 20130101; F01N 3/0842 20130101; F01N 2250/14
20130101; F02D 2041/389 20130101; F01N 3/0231 20130101; F02M 26/28
20160201; F02B 37/00 20130101; F02D 41/0057 20130101; F02D 41/0002
20130101; B01D 53/9495 20130101; F01N 3/0222 20130101; F02D 2250/38
20130101; Y02T 10/40 20130101; F02D 2041/0017 20130101; F01N 3/035
20130101; F02D 41/0055 20130101; F02D 41/029 20130101; F02D
2011/102 20130101; F02D 41/005 20130101; F01N 2570/04 20130101;
F02D 2200/0806 20130101; F02D 2200/602 20130101; F02M 26/47
20160201; F02D 41/0047 20130101; F02D 41/025 20130101; F02D 41/1462
20130101; Y02T 10/12 20130101; F01N 3/023 20130101; F01N 2570/16
20130101; F02D 41/3809 20130101; F01N 3/031 20130101; F01N 11/00
20130101; F01N 2550/04 20130101; F02D 2200/0808 20130101; F01N
3/0871 20130101; F01N 9/002 20130101; F02D 41/0235 20130101; F02D
41/028 20130101; F02M 26/05 20160201; F02D 2200/0804 20130101; F01N
3/0233 20130101 |
Class at
Publication: |
60/277 ; 60/295;
60/297; 60/311 |
International
Class: |
F01N 003/00; F01N
007/00; F01N 003/02 |
Foreign Application Data
Date |
Code |
Application Number |
Jul 24, 2000 |
JP |
2000-227569 |
Jul 24, 2000 |
JP |
2000-227558 |
Apr 27, 2001 |
JP |
2001-133597 |
May 10, 2001 |
JP |
2001-140559 |
Claims
1. An exhaust gas purification apparatus, for an engine having a
combustion chamber, comprising an exhaust passage, a particulate
filter arranged in the exhaust passage for removing particulates in
exhaust gas exhausted from the combustion chamber by oxidation, a
device for controlling characteristic of the exhaust gas flowing
into the particulate filter, and means for judging if the
particulate filter will be deteriorated by heat derived from the
oxidation of the particulates, wherein, when the judging means
judges that the particulate filter will be deteriorated by heat,
the controlling device changes the characteristic of the exhaust
gas flowing into the particulate filter to prevent the particulate
filter from being deteriorated by heat.
2. An exhaust gas purification apparatus, as set forth in claim 1,
wherein the controlling device can control the amount of the
exhaust gas flowing into the particulate filter and wherein, when
the judging means that the particular filter will be deteriorated
by heat, the controlling device performs one of a first control
operation to make the amount of the exhaust gas flowing into the
particulate filter smaller than a first threshold and a second
control operation to make the amount of the exhaust gas flowing
into the particulate filter larger than a second threshold which is
larger than the first threshold.
3. An exhaust gas purification apparatus, as set forth in claim 2,
wherein the apparatus further comprises a bypass mechanism for
making at least a part of the exhaust gas bypass the particulate
filter, and wherein the controlling device makes the amount of the
exhaust gas flowing into the particulate filter smaller than the
first threshold by the bypass mechanism making at least a part of
the exhaust gas bypass the particulate filter.
4. An exhaust gas purification apparatus, as set forth in claim 2,
wherein the controlling device makes the amount of the exhaust gas
flowing into the particulate filter smaller than the first
threshold by reducing the amount of the air taken into the
combustion chamber, and makes the amount of the exhaust gas flowing
into the particulate filter larger than the second threshold by
increasing the amount of the air taken into the combustion
chamber.
5. An exhaust gas purification apparatus, as set forth in claim 4,
wherein the controlling device reduces the amount of the air taken
into the combustion chamber by reducing the engine speed, and
increases the amount of the air taken into the combustion chamber
by increasing the engine speed.
6. An exhaust gas purification apparatus, as set forth in claim 1,
wherein the judging means judges that the particulate filter will
be deteriorated by heat when the temperature of the particulate
filter is higher than a predetermined temperature.
7. An exhaust gas purification apparatus, as set forth in claim 6,
wherein the predetermined temperature is a temperature at which the
particulate is ignited.
8. An exhaust gas purification apparatus, as set forth in claim 1,
wherein the judging means judges that the particulate filter will
be deteriorated by heat when the temperature of the particulate
filter is higher than a predetermined temperature and the
concentration of the oxygen in the exhaust gas is larger than a
predetermined concentration.
9. An exhaust gas purification apparatus, as set forth in claim 8,
wherein the predetermined temperature is a temperature at which the
particulate is ignited.
10. An exhaust gas purification apparatus, as set forth in claim 8,
wherein the predetermined concentration is set to become small as
the concentration of hydrocarbon in the exhaust gas becomes large
when the air-fuel ratio of the exhaust gas is lean, and is set to
become large as the concentration of hydrocarbon in the exhaust gas
becomes large when the air-fuel ratio of the exhaust gas is
stoichiometric or rich.
11. An exhaust gas purification apparatus, as set forth in claim 8,
wherein the predetermined concentration is set to become large as
the amount of the air taken into the combustion chamber becomes
large.
12. An exhaust gas purification apparatus, as set forth in claim 1,
wherein, when the judging means judges that the particulate filter
will be deteriorated by heat, before the characteristic of the
exhaust gas is changed by the controlling device, the judging means
judges if the temperature of the particulate filter will become
lower than the predetermined temperature by changing the
characteristic of the exhaust gas, and if the concentration of the
oxygen in the exhaust gas will become smaller than the
predetermined concentration by changing the characteristic of the
exhaust gas, and the controlling device changes the characteristic
of the exhaust gas to make the temperature of the particulate
filter lower than the predetermined temperature when the judging
means judges that the temperature of the particulate filter will
become lower than the predetermined temperature by changing the
characteristic of the exhaust gas, and the controlling device
changes the characteristic of the exhaust gas to make the
concentration of the oxygen in the exhaust gas smaller than the
predetermined concentration when the judging means judges that the
concentration of the oxygen in the exhaust gas will become smaller
than the predetermined concentration.
13. An exhaust gas purification apparatus, as set forth in claim
12, wherein the controlling device controls the characteristic of
the exhaust gas by controlling the engine operating condition.
14. An exhaust gas purification apparatus, as set forth in claim
12, wherein the apparatus further comprises a bypass mechanism for
making at least a part of the exhaust gas bypass the particulate
filter, and wherein the controlling device makes at least a part of
the exhaust gas bypass the particulate filter by the bypass
mechanism when the judging means judges that, by changing the
characteristic of the exhaust gas, the temperature of the
particulate filter will not become lower than the predetermined
temperature, and the concentration of the oxygen in the exhaust gas
will not become smaller than the predetermined concentration.
15. An exhaust gas purification apparatus, as set forth in claim 1,
wherein the apparatus further comprises a reverse mechanism for
reversing the inflowing direction of the exhaust gas flowing into
the particulate filter.
16. An exhaust gas purification apparatus, as set forth in claim 1,
wherein a precious metal catalyst is carried on the particulate
filter.
17. An exhaust gas purification apparatus, as set forth in claim 1,
wherein an active oxygen release agent which absorbs oxygen and
holds the oxygen when excess oxygen is present in the surroundings
and releases the held oxygen in the form of active oxygen when the
concentration of oxygen in the surroundings falls is carried on the
particulate filter and wherein active oxygen is released from the
active oxygen release agent and the particulates adhering on the
particulate filter are oxidized by the released active oxygen when
the particulates adhere on the particulate filter.
18. An exhaust gas purification apparatus, as set forth in claim
17, wherein the active oxygen release agent is comprised of at
least one of an alkali metal, an alkali earth metal, a rare earth,
a transition metal, and a carbon family element.
19. An exhaust gas purification apparatus, as set forth in claim
18, wherein the alkali metal and alkali earth metal are comprised
of metals higher in tendency toward ionization than calcium.
20. An exhaust gas purification apparatus, as set forth in claim 1,
wherein the particulates adhering on the particulate filter are
oxidized by temporarily making the air-fuel ratio of a part or
whole of the exhaust gas rich.
21. An exhaust gas purification apparatus, as set forth in claim 1,
wherein a NO.sub.x absorbent for absorbing the NO.sub.x in the
exhaust gas when excess oxygen is present in the surroundings and
releases the absorbed NO.sub.x when the concentration of oxygen in
the surroundings falls is carried on the particulate filter and
wherein the characteristic of the exhaust gas flowing into the
particulate filter is returned to the original characteristic when
a predetermined period has elapsed from when the controlling device
changes the characteristic of the exhaust gas, and sulfur adhering
on the particulate filter is disassociated from the particulate
filter by making the air-fuel ratio of a part or the whole of the
exhaust gas rich.
Description
TECHNICAL FIELD
[0001] The present invention relates to an exhaust gas purification
device of an engine.
BACKGROUND ART
[0002] In the related art, in a diesel engine, particulates
contained in the exhaust gas are removed by arranging a particulate
filter in the engine exhaust passage, using that particulate filter
to trap the particulates in the exhaust gas, and igniting and
burning the particulates trapped on the particulate filter to
recycle the particulate filter. The particulates trapped on the
particulate filter, however, do not ignite unless the temperature
becomes as high as at least about 600.degree. C. However, the
temperature of the exhaust gas of a diesel engine is normally
considerably lower than 600.degree. C. Therefore, it is difficult
to use the heat of the exhaust gas to cause the particulates
trapped on the particulate filter to ignite. To use the heat of the
exhaust gas to cause the particulates trapped on the particulate
filter to ignite, it is necessary to lower the ignition temperature
of the particulates.
[0003] It has been known in the related art, however, that the
ignition temperature of particulates can be reduced if a catalyst
is carried on the particulate filter. Therefore, known in the art
are various particulate filters carrying catalysts for reducing the
ignition temperature of the particulates.
[0004] For example, Japanese Examined Patent Publication (Kokoku)
No. 7-106290 discloses a particulate filter comprising a
particulate filter carrying a mixture of a platinum group metal and
an alkali earth metal oxide. In this particulate filter, the
particulates are ignited at a relatively low temperature of about
350.degree. C. to 400.degree. C. and are then continuously
burned.
[0005] Summarizing the problem to be solved by the invention, in a
diesel engine, when the load becomes high, the temperature of the
exhaust gas reaches from 350.degree. C. to 400.degree. C.,
therefore with the above particulate filter, it would appear at
first glance that the particulates could be made to ignite and burn
by the heat of the exhaust gas when the engine load becomes high.
In fact, however, even if the temperature of the exhaust gas
reaches from 350.degree. C. to 400.degree. C., sometimes the
particulates will not ignite. Further, even if the particulates
ignite, only some of the particulates will burn and a large amount
of the particulates will remain unburned.
[0006] That is, when the amount of the particulates contained in
the exhaust gas is small, the amount of the particulates deposited
on the particulate filter is small. At this time, if the
temperature of the exhaust gas reaches from 350.degree. C. to
400.degree. C., the particulates on the particulate filter ignite
and then are continuously burned.
[0007] If the amount of the particulates contained in the exhaust
gas becomes larger, however, before the particulates deposited on
the particulate filter completely burn, other particulates will
deposit on that particulates. As a result, the particulates deposit
in layers on the particulate filter. If the particulates deposit in
layers on the particulate filter in this way, the some of the
particulates easily contacting the oxygen will be burned, but the
remaining particulates which do not contact the oxygen will not
burn and therefore a large amount of particulates will remain
unburned. Therefore, if the amount of particulates contained in the
exhaust gas becomes larger, a large amount of particulates
continues to deposit on the particulate filter.
[0008] On the other hand, if a large amount of particulates is
deposited on the particulate filter, the deposited particulates
gradually become harder to ignite and burn. It probably becomes
harder to burn in this way because the carbon in the particulates
changes to hard-to-burn graphite etc. while being deposited. In
fact, if a large amount of particulates continues to deposit on the
particulate filter, the deposited particulates will not ignite at a
low temperature of 350.degree. C. to 400.degree. C. A high
temperature of over 600.degree.C. is required to cause ignition of
the deposited particulates. In a diesel engine, however, the
temperature of the exhaust gas usually never becomes a high
temperature of over 600.degree. C. Therefore, if a large amount of
particulates continues to deposit on the particulate filter, it is
difficult to cause ignition of the deposited particulates by the
heat of the exhaust gas.
[0009] On the other hand, at this time, if it were possible to make
the temperature of the exhaust gas a high temperature of over
600.degree. C., the deposited particulates would be ignited, but
another problem would occur in this case. That is, in this case, if
the deposited particulates were made to ignite, it would burn while
generating a luminous flame. At this time, the temperature of the
particulate filter would be maintained at over 800.degree. C. for a
long time until the deposited particulates finished being burned.
If the particulate filter is exposed to a high temperature of over
800.degree. C. for a long time in this way, however, the
particulate filter will deteriorate quickly and therefore the
problem will arise of the particulate filter having to be
frequently replaced with a new filter.
DISCLOSURE OF INVENTION
[0010] An object of the present invention is to prevent a
particulate filter of an exhaust purification apparatus from being
deteriorated by heat derived from the burning of the particulates
deposited on the particulate filter.
[0011] According to the present invention, there is provided an
exhaust gas purification apparatus for an engine having a
combustion chamber, comprising an exhaust passage, a particulate
filter arranged in the exhaust passage for removing particulates in
exhaust gas exhausted from the combustion chamber by oxidation, a
device for controlling characteristic of the exhaust gas flowing
into the particulate filter, and means for judging if the
particulate filter will be deteriorated by heat derived from the
oxidation of the particulates, wherein, when the judging means
judges that the particulate filter will be deteriorated by heat,
the controlling device changes the characteristic of the exhaust
gas flowing into the particulate filter to prevent the particulate
filter from being deteriorated by heat.
[0012] According to one embodiment of the invention, the
controlling device can control the amount of the exhaust gas
flowing into the particulate filter and when the judging means
judges that the particular filter will be deteriorated by heat, the
controlling device performs one of a first control operation to
make the amount of the exhaust gas flowing into the particulate
filter smaller than a first threshold, and a second control
operation to make the amount of the exhaust gas flowing into the
particulate filter larger than a second threshold which is larger
than the first threshold.
[0013] According to another embodiment of the invention, when the
judging means judges that the particulate filter will be
deteriorated by heat, before the characteristic of the exhaust gas
is changed by the controlling device, the judging means judges if
the temperature of the particulate filter will become lower than
the predetermined temperature by changing the characteristic of the
exhaust gas, and if the concentration of the oxygen in the exhaust
gas will become smaller than the predetermined concentration by
changing the characteristic of the exhaust gas, and the controlling
device changes the characteristic of the exhaust gas to make the
temperature of the particulate filter lower than the predetermined
temperature when the judging means judges that the temperature of
the particulate filter will become lower than the predetermined
temperature by changing the characteristic of the exhaust gas, and
the controlling device changes the characteristic of the exhaust
gas to make the concentration of the oxygen in the exhaust gas
smaller than the predetermined concentration when the judging means
judges that the concentration of the oxygen in the exhaust gas will
become smaller than the predetermined concentration.
BRIEF DESCRIPTION OF DRAWINGS
[0014] These and other objects and features of the present
invention will be more apparent from the following description
given with reference to the accompanying drawings, wherein:
[0015] FIG. 1 is an overall view of an internal combustion
engine;
[0016] FIGS. 2A and 2B are views of the relationship between a
required torque of an engine, an amount of depression of an
accelerator pedal, and an engine speed;
[0017] FIGS. 3A and 3B are views of a particulate filter;
[0018] FIGS. 4A and 4B are views for explaining an action of
oxidation of particulates;
[0019] FIGS. 5A to 5C are views for explaining an action of
deposition of particulates;
[0020] FIG. 6 is a view of the relationship between the amount of
particulates removable by oxidation and the temperature of the
particulate filter;
[0021] FIGS. 7A and 7B are views of an amount of particulates
removable by oxidation;
[0022] FIGS. 8A to 8F are views of maps of the amount G of
particulates removable by oxidation;
[0023] FIGS. 9A and 9B are views of maps of the concentration of
oxygen and the concentration of NO.sub.x in the exhaust gas;
[0024] FIGS. 10A and 10B are views of the amount of discharged
particulates;
[0025] FIG. 11 is a view of a simultaneous particulate and NO.sub.x
treatment region;
[0026] FIG. 12 is a view for explaining the method of removal by
oxidation of particulates;
[0027] FIG. 13 is a view of the amount of generation of smoke;
[0028] FIGS. 14A and 14B are views of the temperature of gas in the
combustion chamber;
[0029] FIG. 15 is a view of operating regions I and II;
[0030] FIG. 16 is a view of an air-fuel ratio A/F;
[0031] FIG. 17 is a view of a change of an opening degree of a
throttle valve etc.;
[0032] FIG. 18 is a view of a map of an amount of NO.
absorption;
[0033] FIG. 19 is a flow chart for processing a NO.sub.x releasing
flag and SO.sub.x releasing flag;
[0034] FIGS. 20 and 21 are flow charts for control of engine
operation;
[0035] FIG. 22 is a plan view of a bypass mechanism wherein a
rotation position of a switching valve is set at a first rotation
position;
[0036] FIG. 23 is a side view of the bypass mechanism shown in FIG.
21;
[0037] FIG. 24 is a plan view of a bypass mechanism wherein the
rotation position of the switching valve is set at a second
rotation position;
[0038] FIG. 25 is a plan view of the bypass mechanism wherein the
rotation position of the switching valve is set at a neutral
position;
[0039] FIG. 26 a view showing deposited particulates;
[0040] FIG. 27 is a flowchart for controlling the rotation position
of the switching valve;
[0041] FIG. 28 is a flowchart for performing a process for
preventing a thermal deterioration of a first embodiment;
[0042] FIGS. 29A and 29B are maps for showing the relationship
between a safety area, a dangerous area, an amount of intake air,
and a concentration of oxygen;
[0043] FIG. 30 is a flowchart for counting a safety counter;
[0044] FIG. 31 is a flowchart for performing a process for
preventing a thermal deterioration of a second embodiment;
[0045] FIG. 32 is a flowchart for removing deposited
particulates;
[0046] FIG. 33 is a flowchart for preventing the thermal
deterioration;
[0047] FIG. 34 is a flowchart for judging if a thermal
deterioration preventing condition is satisfied; and
[0048] FIG. 35 is a flowchart for judging if a thermal
deterioration preventing condition is satisfied according to
another embodiment.
BEST MODE FOR CARRYING OUT THE INVENTION
[0049] FIG. 1 shows the case of application of the present
invention to a compression ignition type internal combustion
engine. Note that the present invention can also be applied to a
spark ignition type internal combustion engine.
[0050] Referring to FIG. 1, 1 indicates an engine body, 2 a
cylinder block, 3 a cylinder head, 4 a piston, 5 a combustion
chamber, 6 an electrically controlled fuel injector, 7 an intake
valve, 8 an intake port, 9 an exhaust valve, and 10 an exhaust
port. The intake port 8 is connected to a surge tank 12 through a
corresponding intake tube 11, while the surge tank 12 is connected
to a compressor 15 of an exhaust turbocharger 14 through an intake
duct 13. An airflow meter 13a for measuring a flow rate of the
intake air is arranged in an intake pipe 13b upstream of the
compressor 15. Inside the intake duct 13 is arranged a throttle
valve 17 driven by a step motor 16. Further, a cooling device 18 is
arranged around the intake duct 13 for cooling the intake air
flowing through the intake duct 13. In the embodiment shown in FIG.
1, the engine coolant water flows inside the cooling device 18 and
the intake air is cooled by the engine coolant water. On the other
hand, the exhaust port 10 is connected to an exhaust turbine 21 of
an exhaust turbocharger 14 through an exhaust manifold 19 and an
exhaust pipe 20. The outlet of the exhaust turbine 21 is connected
to a casing 23 housing a particulate filter 22 through an exhaust
pipe 20a.
[0051] The exhaust manifold 19 and the surge tank 12 are connected
to each other through an exhaust gas recirculation (EGR) passage
24. Inside the EGR passage 24 is arranged an electrically
controlled EGR control valve 25. A cooling device 26 is arranged
around the EGR passage 24 to cool the EGR gas circulating inside
the EGR passage 24. In the embodiment shown in FIG. 1, the engine
coolant water is guided inside the cooling device 26 and the EGR
gas is cooled by the engine coolant water. On the other hand, fuel
injectors 6 are connected to a fuel reservoir, a so-called common
rail 27, through fuel feed pipes 6a. Fuel is fed into the common
rail 27 from an electrically controlled variable discharge fuel
pump 28. The fuel fed into the common rail 27 is fed to the fuel
injectors 6 through the fuel.feed pipes 6a. The common rail 29 has
a fuel pressure sensor 29 attached to it for detecting the fuel
pressure in the common rail 27. The discharge of the fuel pump 28
is controlled based on the output signal of the fuel pressure
sensor 29 so that the fuel pressure in the common rail 27 becomes a
target fuel pressure.
[0052] An electronic control unit 30 is comprised of a digital
computer provided with a read only memory (ROM) 32, random access
memory (RAM) 33, microprocessor (CPU) 34, input port 35, and output
port 36 connected to each other through a bidirectional bus 31. The
output signal of the fuel pressure sensor 29 is input through a
corresponding AD converter 37 to the input port 35. Further, the
particulate filter 22 has attached to it a temperature sensor 39
for detecting the particulate filter 22. The output signal of this
temperature sensor 39 is input to the input port 35 through the
corresponding AD converter 37. The output signal of the airflow
meter 13a is input into the input port 35 through the corresponding
AD converter 37. An accelerator pedal 40 has connected to it a load
sensor 41 generating an output voltage proportional to the amount
of depression L of the accelerator pedal 40. The output voltage of
the load sensor 41 is input to the input port 35 through the
corresponding AD converter 37. Further, the input port 35 has
connected to it a crank angle sensor 42 generating an output pulse
each time a crankshaft rotates by for example 30 degrees. On the
other hand, the output port 36 is connected through corresponding
drive circuits 38 to the fuel injectors 6, the step motor 16 for
driving the throttle valve, the EGR control valve 25, and the fuel
pump 28.
[0053] FIG. 2A shows the relationship between the required torque
TQ, the amount of depression L of the accelerator pedal 40, and the
engine speed N. Note that in FIG. 2A, the curves show the
equivalent torque curves. The curve shown by TQ=O shows the torque
at zero, while the remaining curves show gradually increasing
required torques in the order of TQ=a, TQ=b, TQ=c, and TQ=d. The
required torque TQ shown in FIG. 2A, as shown in FIG. 2B, is stored
in the ROM 32 in advance as a function of the amount of depression
L of the accelerator pedal 40 and the engine speed N. In this
embodiment of the present invention, the required torque TQ in
accordance with the amount of depression L of the accelerator pedal
40 and the engine speed N is first calculated from the map shown in
FIG. 2B, then the amount of fuel injection, etc. are calculated
based on the required torque TQ.
[0054] FIGS. 3A and 3B show the structure of the particulate filter
22. Note that FIG. 3A is a front view of the particulate filter 22,
while FIG. 3B is a side sectional view of the particulate filter
22. As shown in FIGS. 3A and 3B, the particulate filter 22 forms a
honeycomb structure and is provided with a plurality of exhaust
circulation passages 50, 51 extending in parallel with each other.
These exhaust circulation passages comprise exhaust gas inflow
passages 50 with downstream ends sealed by plugs 52 and exhaust gas
outflow passages 51 with upstream ends sealed by plugs 52. Note
that the hatched portions in FIG. 3A show plugs 53. Therefore, the
exhaust gas inflow passages 50 and the exhaust gas outflow passages
51 are arranged alternately through thin wall partitions 54. In
other words, the exhaust gas inflow passages 50 and the exhaust gas
outflow passages 51 are arranged so that each exhaust gas inflow
passage 50 is surrounded by four exhaust gas outflow passages 51,
and each exhaust gas outflow passage 51 is surrounded by four
exhaust gas inflow passages 50.
[0055] The particulate filter 22 is formed from a porous material
such as, for example, cordierite. Therefore, the exhaust gas
flowing into the exhaust gas inflow passages 50 flows out into the
adjoining exhaust gas outflow passages 51 through the surrounding
partitions 54 as shown by the arrows in FIG. 3B.
[0056] In an embodiment of the present invention, a layer of a
carrier comprised of for example alumina is formed on the
peripheral surfaces of the exhaust gas inflow passages 50 and the
exhaust gas outflow passages 51, that is, the two side surfaces of
the partitions 54, the inside walls of the fine holes in the
partitions 54 outer end faces of the plugs 53, and inner end face
of the plugs 52, 53. On the carrier are carried a precious metal
catalyst and an active oxygen release agent which absorbs the
oxygen and holds the oxygen if excess oxygen is present in the
surroundings and releases the held oxygen in the form of active
oxygen if the concentration of the oxygen in the surroundings
falls.
[0057] In this case, in an embodiment according to the present
invention, platinum Pt is used as the precious metal catalyst. As
the active oxygen release agent, use is made of at least one of an
alkali metal such as potassium K, sodium Na, lithium Li, cesium Cs,
and rubidium Rb, an alkali earth metal such as barium Ba, calcium
Ca, and strontium Sr, a rare earth such as lanthanum La, yttrium Y,
and cerium Ce, a transition metal such as iron Fe, and a carbon
family element such as tin Sn.
[0058] Note that in this case, as the active oxygen release agent,
use is preferably made of an alkali metal or an alkali earth metal
with a higher tendency to ionization than calcium Ca, that is,
potassium K, lithium Li, cesium Cs, rubidium Rb, barium Ba, and
strontium Sr.
[0059] Next, the action of removal of the particulates in the
exhaust gas by the particulate filter 22 will be explained by
taking, as an example, the case of carrying platinum Pt and
potassium K on a carrier, but the same type of action for removal
of particulates is performed even when using another precious
metal, alkali metal, alkali earth metal, rare earth, transition
metal and carbon family element.
[0060] In a compression ignition type internal combustion engine
such as shown in FIG. 1, combustion occurs under an excess of air.
Therefore, the exhaust gas contains a large amount of excess air.
That is, if the ratio of the air and fuel fed into the intake
passage, combustion chamber 5, and exhaust passage is called the
air-fuel ratio of the exhaust gas, then in a compression ignition
type internal combustion engine such as shown in FIG. 1, the
air-fuel ratio of the exhaust gas becomes lean. Further, in the
combustion chamber 5, NO is generated, so the exhaust gas contains
NO. Further, the fuel contains sulfur S. This sulfur S reacts with
the oxygen in the combustion chamber 5 to become SQ.sub.2.
Therefore, the exhaust gas contains SQ.sub.2. Accordingly, exhaust
gas containing excess oxygen, NO.sub.x and SO.sub.2 flows into the
exhaust gas inflow passages 50 of the particulate filter 22. FIGS.
4A and 4B are enlarged views of the surface of the carrier layer
formed on the inner circumferential surfaces of the exhaust gas
inflow passages 50 and the inside walls of the fine holes in the
partitions 54. Note that in FIGS. 4A and 4B, 60 indicates particles
of platinum Pt, while 61 indicates the active oxygen release agent
containing potassium K.
[0061] In this way, since a large amount of excess oxygen is
contained in the exhaust gas, if the exhaust gas flows into the
exhaust gas inflow passages 50 of the particulate filter 22, as
shown in FIG. 4A, the oxygen O.sub.2 adheres to the surface of the
platinum Pt in the form of O.sub.2.sup.- or O.sup.2-. On the other
hand, the NO in the exhaust gas reacts with the O.sub.2.sup.- or
O.sup.2- on the surface of the platinum Pt to become NO.sub.2
(2NO+O.sub.2.fwdarw.2NO.sub.2). Next, part of the NO.sub.2 which is
produced is absorbed in the active oxygen release agent 61 while
being oxidized on the platinum Pt and diffuses in the active oxygen
release agent 61 in the. form of nitrate ions NO.sub.3.sup.31 as
shown in FIG. 4A. Part of the nitrate ions NO.sub.3.sup.31 produces
potassium nitrate KNO.sub.3.
[0062] On the other hand, as explained above, the exhaust gas also
contains SO.sub.2. This SO.sub.2 is absorbed in the active oxygen
release agent 61 by a mechanism similar to that of NO. That is, in
the above way, the oxygen O.sub.2 adheres to the surface of the
platinum Pt in the form of O.sub.2.sup.- or O.sup.2-. The SO.sub.2
in the exhaust gas reacts with the O.sub.2- or O.sub.2.sup.- on the
surface of the platinum Pt to become SO.sub.3. Next, part of the
SO.sub.3 which is produced is absorbed in the active oxygen release
agent 61 while being oxidized on the platinum Pt and diffuses in
the active oxygen release agent 61 in the form of sulfate ions
SO.sub.4.sup.2- while bonding with the potassium K to produce
potassium sulfate K.sub.2SO.sub.4. In this way, potassium sulfate
KNO.sub.3 and potassium sulfate K.sub.2SO.sub.4 are produced in the
active oxygen release agent 61.
[0063] On the other hand, particulates comprised of mainly carbon
are produced in the combustion chamber 5. Therefore, the exhaust
gas contains these particulates. The particulates contained in the
exhaust gas contact and adhere to the surface of the carrier layer,
for example, the surface of the active oxygen release agent 61, as
shown in FIG. 4B, when the exhaust gas is flowing through the
exhaust gas inflow passages 50 of the particulate filter 22 or when
moving from the exhaust gas inflow passages 50 to the exhaust gas
outflow passages 51.
[0064] If the particulate 62 adheres to the surface of the active
oxygen release agent 61 in this way, the concentration of oxygen at
the contact surface of the particulate 62 and the active oxygen
release agent 61 falls. If the concentration of oxygen falls, a
difference in concentration occurs with the inside of the high
oxygen concentration active oxygen release agent 61 and therefore
the oxygen in the active oxygen release agent 61 moves toward the
contact surface between the particulate 62 and the active oxygen
release agent 61. As a result, the potassium nitrate KNO.sub.3
formed in the active oxygen release agent 61 is broken down into
potassium K, oxygen O, and NO. The oxygen O moves toward the
contact surface between the particulate 62 and the active oxygen
release agent 61, while the NO is released from the active oxygen
release agent 61 to the outside. The NO released to the outside is
oxidized on the downstream side platinum Pt and is again absorbed
in the active oxygen release agent 61.
[0065] On the other hand, if the temperature of the particulate
filter 22 is high at this time, the potassium sulfate
K.sub.2SO.sub.4 formed in the active oxygen release agent 61 is
also broken down into potassium K, oxygen O, and SO.sub.2. The
oxygen O moves toward the contact surface between the particulate
62 and the active oxygen release agent 61, while the SO.sub.2 is
released from the active oxygen release agent 61 to the outside.
The SO.sub.2 released to the outside is oxidized on the downstream
side platinum Pt and again absorbed in the active oxygen release
agent 61. Note that, since the potassium sulfate K.sub.2SO.sub.4 is
stable and hard to break down, the potassium sulfate
K.sub.2SO.sub.4 releases the active oxygen less than does the
potassium nitrate KNO.sub.3.
[0066] Further, as explained above, the active oxygen release agent
61 produces and releases the active oxygen during the reaction with
the oxygen when the active oxygen release agent 61 absorbs NO.sub.x
in the form of nitrate ions NO.sub.3.sup.-. Similarly, the active
oxygen release agent 61 produces and releases the active oxygen
during the reaction with the oxygen when the active oxygen release
agent 61 absorbs SO.sub.2 in the form of sulfate ions
SO.sub.4.sup.2-.
[0067] On the other hand, the oxygen O moving toward the contact
surface between the particulate 62 and the active oxygen release
agent 61 is the oxygen broken down from compounds such as potassium
nitrate KNO.sub.3 or potassium sulfate K.sub.2SO.sub.4. The oxygen
O broken down from these compounds has a high energy and has an
extremely high activity. Therefore, the oxygen moving toward the
contact surface between the particulate 62 and the active oxygen
release agent 61 becomes active oxygen O. Similarly, oxygen
produced during the reaction of NO.sub.x or SO.sub.2 with oxygen in
the active oxygen release agent 61 becomes active oxygen O. If this
active oxygen O. contacts the particulate 62, the oxidation action
of the particulate 62 is promoted and the particulate 62 is
oxidized without emitting a luminous flame for a short period of
several seconds to several tens of minutes and is completely
removed. While the particulate 62 is being oxidized in this way,
other particulate are successively depositing on the particulate
filter 22. Therefore, in practice, a certain amount of particulates
is always depositing on the particulate filter 22. Part of the
deposited particulates are removed by oxidation. In this way, the
particulates 62 deposited on the particulate filter 22 are
continuously burned without emitting luminous flame.
[0068] Note that the NO.sub.x is considered to diffuse in the
active oxygen release agent 61 in the form of nitrate ions
NO.sub.3.sup.- while repeatedly bonding with and separating from
the oxygen atoms. Active oxygen is produced during this time as
well. The particulates 62 are also oxidized by this active oxygen.
Further, the particulate 62 deposited on the particulate filter 22
is oxidized by the active oxygen O, but the particulate 62 is also
oxidized by the oxygen in the exhaust gas.
[0069] Further, note that the active oxygen release agent 61 is a
material for oxidizing the particulates.
[0070] When the particulates deposited in layers on the particulate
filter 22 are burned, the particulate filter 22 becomes red hot and
burns with a flame. This burning with a flame does not continue
unless the temperature is high. Therefore, to continue burning with
a flame, the temperature of the particulate filter 22 must be
maintained high.
[0071] As opposed to this, in the present invention, the
particulates 62 are oxidized without emitting a luminous flame as
explained above. At this time, the surface of the particulate
filter 22 does not become red hot. That is, in other words, in the
present invention, the particulates 62 are removed by oxidation at
a considerably low temperature. Accordingly, the action of removal
of the particulates 62 by oxidation without emitting a luminous
flame according to the present invention is completely different
from the action of removal of particulates by burning accompanied
with a flame.
[0072] The platinum Pt and the active oxygen release agent 61
become more active the higher the temperature of the particulate
filter 22, so the amount of the active oxygen O which can be
released by the active oxygen release agent 61 per unit time
increases the higher the temperature of the particulate filter 22.
Further, naturally, the particulates are more easily removed, by
oxidation, the higher the temperature of the particulates itself.
Therefore, the amount of the particulates removable by oxidation
per unit time, without emitting a luminous flame on the particulate
filter 22, increases the higher the temperature of the particulate
filter 22.
[0073] The solid line in FIG. 6 shows the amount G of the
particulates removable by oxidation per unit time without emitting
a luminous flame. The abscissa of FIG. 6 shows the temperature TF
of the particulate filter 22. Note that FIG. 6 shows the amount G
of particulates removable by oxidation in the case where the unit
time is 1 second, that is, per second, but 1 minute, 10 minutes, or
any other time may also be employed as the unit time. For example,
when using 10 minutes as the unit time, the amount G of
particulates removable by oxidation per unit time expresses the
amount G of particulates removable by oxidation per 10 minutes. In
this case as well, the amount G of particulates removable by
oxidation per unit time, without emitting a luminous flame on the
particulate filter 22, as shown in FIG. 6, increases the higher the
temperature of the particulate filter 22.
[0074] Now, if the amount of the particulates discharged from the
combustion chamber 5 per unit time is called the amount M of
discharged particulates, when the amount M of discharged
particulates is smaller than the amount G of particulates removable
by oxidation for the same unit time or when the amount M of
discharged particulates per 10 minutes is smaller than the amount G
of particulates removable by oxidation per 10 minutes, that is, in
the region I of FIG. 6, all of the particulates discharged from the
combustion chamber 5 and contacting the particulate filter 22 is
removed by oxidation successively in a short time without emitting
a luminous flame on the particulate filter 22.
[0075] As opposed to this, when the amount M of discharged
particulates is larger than the amount G of particulates removable
by oxidation, that is, in the region II of FIG. 6, the amount of
active oxygen is not sufficient for successive oxidation of all of
the particulates. FIGS. 5A to 5C show the state of oxidation of
particulates in this case.
[0076] That is, when the amount of active oxygen is not sufficient
for successive oxidation of all of the particulates, if
particulates 62 adhere on the active oxygen release agent 61 as
shown in FIG. 5A, only some of the particulates 62 are oxidized.
The portions of the particulates not sufficiently oxidized remain
on the carrier layer. Next, if the state of insufficient amount of
active oxygen continues, the portions of the particulates not
oxidized successively remain on the carrier layer. As a result, as
shown in FIG. 5B, the surface of the carrier layer is covered by
the residual particulate portions 63.
[0077] This residual particulate portion 63 covering the surface of
the carrier layer gradually changes to hard-to-oxidize graphite and
therefore the residual particulate portion 63 easily remains as it
is. Further, if the surface of the carrier layer is covered by the
residual particulate portion 63, the action of oxidation of the NO
and SO.sub.2 by the platinum Pt and the action of release of the
active oxygen from the active oxygen release agent 61 are
suppressed. As a result, as shown in FIG. 5C, other particulates 64
successively deposit on the residual particulate portion 63. That
is, the particulates deposit in layers. If the particulates deposit
in layers in this way, the particulates are separated in distance
from the platinum Pt or the active oxygen release agent 61, so even
if they are easily oxidizable particulates, they will not be
oxidized by active oxygen O. Therefore, other particulates
successively deposit on the particulate 64. That is, if the state
of the amount M of discharged particulates being larger than the
amount G of particulates removable by oxidation continues,
particulates deposit in layers on the particulate filter 22 and,
therefore, unless the temperature of the exhaust gas is made higher
or the temperature of the particulate filter 22 is made higher, it
is no longer possible to cause the deposited particulates to ignite
and burn.
[0078] In this way, in the region I of FIG. 6, the particulates are
burned in a short time without emitting a luminous flame on the
particulate filter 22. In the region II of FIG. 6, the particulates
deposit in layers on the particulate filter 22. Therefore, to
prevent the particulates from depositing in layers on the
particulate filter 22, the amount M of discharged particulates has
to be kept smaller than the amount G of the particulates removable
by oxidation at all times.
[0079] As will be understood from FIG. 6, with the particulate
filter 22 used in this embodiment of the present invention, the
particulates can be oxidized even if the temperature TF of the
particulate filter 22 is considerably low. Therefore, in a
compression ignition type internal combustion engine shown in FIG.
1, it is possible to maintain the amount M of the discharged
particulates and the temperature TF of the particulate filter 22 so
that the amount M of discharged particulates normally becomes
smaller than the amount G of the particulates removable by
oxidation. Therefore, in this embodiment of the present invention,
the amount M of discharged particulates and the temperature TF of
the particulate filter 22 are maintained so that the amount M of
discharged particulates usually becomes smaller than the amount G
of the particulates removable by oxidation.
[0080] If the amount M of discharged particulates is maintained to
be usually smaller than the amount G of particulates removable by
oxidation in this way, the particulates no longer deposit in layers
on the particulate filter 22. As a result, the pressure loss of the
flow of exhaust gas in the particulate filter 22 is maintained at a
substantially constant minimum pressure loss to the extent of not
changing much at all. Therefore, it is possible to maintain the
drop in output of the engine at a minimum.
[0081] Further, the action of removal of particulates by oxidation
of the particulates takes place even at a considerably low
temperature. Therefore, the temperature of the particulate filter
22 does not rise that much at all and consequently there is almost
no risk of deterioration of the particulate filter 22. Further,
since the particulates do not deposit in layers on the particulate
filter 22, there is no danger of coagulation of ash and therefore
there is less danger of the particulate filter 22 clogging.
[0082] This clogging however occurs mainly due to the calcium
sulfate CaSO.sub.4. That is, fuel or lubrication oil contains
calcium Ca. Therefore, the exhaust gas contains calcium Ca. This
calcium Ca produces calcium sulfate CaSO.sub.4 in the presence of
SO.sub.3. This calcium sulfate CaSO.sub.4 is a solid and will not
break down by heat even at a high temperature. Therefore, if
calcium sulfate CaSO.sub.4 is produced and the fine holes of the
particulate filter 22 are clogged by this calcium sulfate
CaSO.sub.4, clogging occurs.
[0083] In this case, however, if an alkali metal or an alkali earth
metal having a higher tendency toward ionization than calcium Ca,
for example potassium K, is used as the active oxygen release agent
61, the SO.sub.3 diffused in the active oxygen release agent 61
bonds with the potassium K to form potassium sulfate
K.sub.2SO.sub.4. The calcium Ca passes through the partitions 54 of
the particulate filter 22 and flows out into the exhaust gas
outflow passage 51 without bonding with the SO.sub.3. Therefore,
there is no longer any clogging of fine holes of the particulate
filter 22. Accordingly, as described above, it is preferable to use
an alkali metal or an alkali earth metal having a higher tendency
toward ionization than calcium Ca, that is, potassium K, lithium
Li, cesium Cs, rubidium Rb, barium Ba, and strontium Sr, as the
active oxygen release agent 61.
[0084] In an embodiment of the present invention, the intention is
basically to maintain the amount M of the discharged particulates
smaller than the amount G of the particulates removable by
oxidation in all operating states. In practice, however, it is
almost impossible to keep the amount X of discharged particulates
lower than the amount G of the particulates removable by oxidation
in all operating states. For example, at the time of engine
startup, the temperature of the particulate filter 22 is normally
low. Therefore, at this time, the amount M of discharged
particulates becomes larger than the amount G of the particulates
removable by oxidation. Therefore, in this embodiment of the
present invention, the amount M of discharged particulates is made
to become smaller than the amount G of the particulates removable
by oxidation normally continuously except for special cases such as
right after engine startup.
[0085] Note that if the amount M of discharged particulates becomes
larger than the amount G of the particulates removable by oxidation
such as immediately after engine startup, the portion of the
particulate which could not be oxidized on the particulate filter
22 remaining. If the amount M of discharged particulates becomes
smaller than the amount G of the particulates removable by
oxidation when this portion of the particulate which could not be
oxidized in this way remains, that is, when the particulates only
deposit less than a certain limit, the portion of the residual
particulate is removed by oxidation by the active oxygen O without
emitting a luminous flame. Therefore, in this embodiment of the
present invention, at the time of a special operating state such as
immediately after engine startup, the amount M of discharged
particulates and the temperature TF of the particulate filter 22
are maintained so that only an amount of particulates, less than a
certain limit which can be removed by oxidation when the amount M
of discharged particulates becomes smaller than the amount G of the
particulates removable by oxidation, deposits on the particulate
filter 22.
[0086] Further, there are sometimes cases where the particulates
deposit in layers on the particulate filter 22 due to some reason
or another even if the amount M of discharged particulates and the
temperature TF of the particulate filter 22 are maintained in this
way. Even in this case, if the air-fuel ratio of part or all of the
exhaust gas is made temporarily rich, the particulates deposited on
the particulate filter 22 is oxidized without emitting a luminous
flame. That is, if the air-fuel ratio of the exhaust gas is made
rich, that is, if the concentration of oxygen in the exhaust gas is
lowered, the active oxygen O is released all at once to the outside
from the active oxygen release agent 61. The particulates deposited
by the active oxygen O released all at once is removed by oxidation
in a short time without emitting a luminous flame.
[0087] On the other hand, if the air-fuel ratio is maintained lean,
the surface of the platinum Pt is covered by oxygen and so-called
oxygen poisoning of the platinum Pt occurs. If such oxygen
poisoning occurs, the action of oxidation of the NO.sub.x falls, so
the efficiency of NO.sub.x absorption falls and therefore the
amount of active oxygen released from the active oxygen release
agent 61 falls. If the-air-fuel ratio is made rich, however, the
oxygen on the surface of the platinum Pt is consumed, so the oxygen
poisoning is eliminated. Therefore, if the air-fuel ratio is
changed from rich to lean, the action of oxidation of the NO.sub.x
becomes stronger, so the efficiency of NO.sub.x absorption becomes
higher and therefore the amount of release of active oxygen from
the active oxygen release agent 61 increases.
[0088] Therefore, if the air-fuel ratio is sometimes switched from
lean to rich when the air-fuel ratio is maintained lean, the oxygen
poisoning of the platinum Pt is eliminated each time. Therefore the
amount of release of active oxygen increases when the air-fuel
ratio is lean and therefore the action of oxidation of the
particulates on the particulate filter 22 can be promoted.
[0089] Now, in FIG. 6, the amount G of the particulates removable
by oxidation is shown as a function of only the temperature TF of
the particulate filter 22, but the amount G of the particulates
removable by oxidation is actually a function of the concentration
of oxygen in the exhaust gas, the concentration of NO.sub.x in the
exhaust gas, the concentration of unburned hydrocarbons in the
exhaust gas, the degree of ease of oxidation of the particulates,
the spatial velocity of the flow of exhaust gas in the particulate
filter 22, the pressure of the exhaust gas, etc. Therefore, the
amount G of the particulates removable by oxidation is preferably
calculated taking into consideration the effects of all of the
above factors including the temperature TF of the particulate
filter 22.
[0090] The factor having the greatest effect on the amount G of the
particulates removable by oxidation among these however is the
temperature TF of the particulate filter 22. Factors having
relatively large effects are the concentration of oxygen in the
exhaust gas and the concentration of NO.sub.x. FIG. 7A shows the
change of the amount G of the particulates removable by oxidation
when the temperature TF of the particulate filter 22 and the
concentration of oxygen in the exhaust gas change. FIG. 7B shows
the change of the amount G of the particulates removable by
oxidation when the temperature TF of the particulate filter 22 and
the concentration of NO.sub.x in the exhaust gas change. Note that,
in FIGS. 7A and 7B, the broken lines show the cases when the
concentration of oxygen and the concentration of NO.sub.x in the
exhaust gas are the reference values. In FIG. 7A, [O.sub.2].sub.1
shows the case when the concentration of oxygen in the exhaust gas
is higher than the reference value, while [O.sub.2].sub.2 shows the
case where the concentration of oxygen is even higher than
[O.sub.2].sub.1 In FIG. 7B, [NO].sub.1 shows the case when the
concentration of NO.sub.x in the exhaust gas is higher than the
reference value, while [NO] .sub.2 shows the case where the
concentration of NO.sub.x is even higher than [NO].sub.1.
[0091] If the concentration of oxygen in the exhaust gas becomes
high, the amount G of the particulates removable by oxidation
increases. Since the amount of oxygen absorbed into the active
oxygen release agent 61 further increases, however, the active
oxygen released from the active oxygen release agent 61 also
increases. Therefore, as shown in FIG. 7A, the higher the
concentration of oxygen in the exhaust gas, the more the amount G
of the particulates removable by oxidation increases.
[0092] On the other hand, the NO in the exhaust gas, as explained
earlier, is oxidized on the surface of the platinum Pt and becomes
NO.sub.2. Part of the thus produced NO.sub.2 is absorbed in the
active oxygen release agent 61, while the remaining NO.sub.2
disassociates to the outside from the surface of the platinum Pt.
At this time, if the platinum Pt contacts the NO.sub.2, an
oxidation reaction will be promoted. Therefore, as shown in FIG.
7B, the higher the concentration of NO.sub.x in the exhaust gas,
the more the amount G of the particulates removable by oxidation
increases. However, the action of promoting the oxidation of the
particulates by the NO.sub.2 only occurs while the temperature of
the exhaust gas is from about 250.degree. C. to about 450.degree.
C., so, as shown in FIG. 7B, if the concentration of NO.sub.x in
the exhaust gas becomes higher, the amount G of the particulates
removable by oxidation increases while the temperature TF of the
particulate filter 22 is from about 250.degree. C. to 450.degree.
C.
[0093] As explained above, it is preferable to calculate the amount
G of the particulates removable by oxidation taking into
consideration all of the factors having an effect on the amount G
of the particulates removable by oxidation. In this embodiment of
the present invention, however, the amount G of the particulates
removable by oxidation is calculated based on only the temperature
TF of the particulate filter 22 having the largest effect on the
amount G of the particulates removable by oxidation among the
factors and the concentration of oxygen and the concentration of
NO.sub.x in the exhaust gas having relatively large effects.
[0094] That is, in this embodiment of the present invention, as
shown in FIG. 8A to 8F, the amounts G of particulates removable by
oxidation at various temperatures TF (200.degree. C., 250.degree.
C., 300.degree. C., 350.degree. C., 400.degree. C., and 450.degree.
C.) are stored in advance in the ROM 32 in the form of a map as a
function of the concentration of oxygen [O.sub.2] in the exhaust
gas and the concentration of NO.sub.x [NO] in the exhaust gas. The
amount G of the particulates removable by oxidation in accordance
with the temperature TF of the particulate filter 22, the
concentration of oxygen [O.sub.2], and the concentration of
NO.sub.x [NO] is calculated by proportional distribution from the
maps shown from FIGS. 8A to 8F.
[0095] Note that the concentration of oxygen [O.sub.2] and the
concentration of NO.sub.x [NO] in the exhaust gas can be detected
using an oxygen concentration sensor and a NO.sub.x concentration
sensor. In this embodiment of the present invention, however, the
concentration of oxygen [O.sub.2] in the exhaust gas is stored in
advance in the ROM 32 in the form of a map as shown in FIG. 9A as a
function of the required torque TQ and engine speed N. The
concentration of NO.sub.x [NO] in the exhaust gas is stored in
advance in the ROM 32 in the form of a map as shown in FIG. 9B as a
function of the required torque TQ and the engine speed N. The
concentration of oxygen [O.sub.2] and concentration of NO.sub.x
[NO] in the exhaust gas are calculated from these maps.
[0096] On the other hand, the amount G of the particulates
removable by oxidation changes according to the type of the engine,
but once the type of the engine is determined, it becomes a
function of the required torque TQ and the engine speed N. FIG. 10A
shows the amount M of discharged particulates of the internal
combustion engine shown in FIG. 1. The curves M.sub.1, M.sub.2,
M.sub.3, M.sub.4, and M.sub.5 show the amounts of equivalent
discharged particulates (M.sub.1<M.sub.2<M.sub.3<M-
.sub.4<M.sub.5). In the example shown in FIG. 10A, the higher
the required torque TQ, the more the amount M of discharged
particulates increases. Note that the amount M of discharged
particulates shown in FIG. 10A is stored in advance in the ROM 32
in the form of a map shown in FIG. 10B as a function of the
required torque TQ and the engine speed N.
[0097] Now, in the embodiment according to the present invention,
as explained above, a layer of a carrier comprised of aluminum is,
for example, formed on the two side surfaces of the partitions 54
of the particulate filter 22 and the inside walls of the fine holes
in the partitions 54. A precious metal catalyst and active oxygen
release agent are carried on this carrier. Further, in this
embodiment of the present invention, the carrier carries a precious
metal catalyst and an NO.sub.x absorbent which absorbs the NO.sub.x
contained in the exhaust gas when the air-fuel ratio of the exhaust
gas flowing into the particulate filter 22 is lean and releases the
absorbed NO.sub.x when the air-fuel ratio of the exhaust gas
flowing into the particulate filter 22 becomes the stoichiometric
air-fuel ratio or rich.
[0098] In this embodiment according to the present invention,
platinum Pt is used as the precious metal catalyst. As the NO.sub.x
absorbent, use is made of at least one of an alkali metal such as
potassium K, sodium Na, lithium Li, cesium Cs, and rubidium Rb, an
alkali earth metal such as barium Ba, calcium Ca, and strontium Sr,
and a rare earth such as lanthanum La and yttrium Y. Note that, as
will be understood by a comparison with the metal comprising the
above active oxygen release agent, the metal comprising the
NO.sub.x absorbent and the metal comprising the active oxygen
release agent match, in large part.
[0099] In this case, it is possible to use different metals or to
use the same metal as the NO.sub.x absorbent and the active oxygen
release agent. When using the same metal as the NO.sub.x absorbent
and the active oxygen release agent, the function as a NO.sub.x
absorbent and the function of an active oxygen release agent are
simultaneously exhibited.
[0100] Next, an explanation will be given of the action of
absorption and release of NO.sub.x taking, as an example, the case
of use of platinum Pt as the precious metal catalyst and use of
potassium K as the NO.sub.x absorbent.
[0101] First, considering the action of absorption of NO.sub.x, the
NO.sub.x is absorbed in the NO.sub.x absorbent by the same
mechanism as the mechanism shown in FIG. 4A. However, in this case,
in FIG. 4A, reference numeral 61 indicates the NO.sub.x
absorbent.
[0102] When the air-fuel ratio of the exhaust gas flowing into the
particulate filter 22 is lean, since a large amount of excess
oxygen is contained in the exhaust gas, if the exhaust gas flows
into the exhaust gas inflow passages 50 of the particulate filter
22, as shown in FIG. 4A, the oxygen O.sub.2adheres to the surface
of the platinum Pt in the form of O.sub.2.sup.- or O.sup.2-. On the
other hand, the NO in the exhaust gas reacts with the O.sub.2.sup.-
or O.sup.2-on the surface of the platinum Pt to become NO.sub.2
(2NO+O.sub.2.fwdarw.2NO.sub.2). Next, part of the NO.sub.2 which is
produced is absorbed in the NO.sub.x absorbent 61 while being
oxidized on the platinum Pt and diffuses in the NO.sub.x absorbent
61 in the form of nitrate ions NO.sub.3.sup.- as shown in FIG. 4A
while bonding with the potassium K. Some of the nitrate ions
NO.sub.3.sup.-produce potassium nitrate KNO.sub.3. In this way, NO
is absorbed in the NO.sub.x absorbent 61. On the other hand, when
the exhaust gas flowing into the particulate filter 22 becomes
rich, the nitrate ions NO.sub.3.sup.- are broken down into oxygen O
and NO and then NO is successively released from the NO.sub.x
absorbent 61. Therefore, when the air-fuel ratio of the exhaust gas
flowing into the particulate filter 22 becomes rich, the NO is
released from the NO.sub.x absorbent 61 in a short time. Further,
the released NO is reduced, so no NO is discharged into the
atmosphere.
[0103] Note that in this case, even if the air-fuel ratio of the
exhaust gas flowing into the particulate filter 22 is the
stoichiometric air-fuel ratio, NO is released from the NO.sub.x
absorbent 61. In this case, however, since the NO is only released
gradually from the NO.sub.x absorbent 61, it takes a somewhat long
time for all of the NO.sub.x absorbed in the NO.sub.x absorbent 61
to be released.
[0104] As explained above, however, it is possible to use different
metals for the NO.sub.x absorbent and the active oxygen release
agent. In this embodiment of the present invention, however, the
same metal is used for the NO.sub.x absorbent and the active oxygen
release agent. In this case, as explained earlier, the function of
the NO.sub.x absorbent and the function of the active oxygen
release agent are performed simultaneously. An agent which performs
these two functions simultaneously will be called an active oxygen
release agent/NO.sub.x absorbent from here on. Therefore, in this
embodiment of the present invention, reference numeral 61 in FIG.
4A shows an active oxygen release agent/NO.sub.x absorbent.
[0105] When using such an active oxygen release agent/NO.sub.x
absorbent, when the air-fuel ratio of the exhaust gas flowing into
the particulate filter 22 is lean, the NO contained in the exhaust
gas is absorbed in the active oxygen release agent/NO.sub.x
absorbent 71. If the particulates contained in the exhaust gas
adhere to the active oxygen release agent/NO.sub.x absorbent 61,
the particulates are removed by oxidation in a short time by the
active oxygen contained in the exhaust gas and the active oxygen
released from the active oxygen release agent/NO.sub.x absorbent
61. Therefore, at this time, it is possible to prevent the
discharge of both the particulates and the NO.sub.x in the exhaust
gas into the atmosphere.
[0106] On the other hand, when the air-fuel ratio of the exhaust
gas flowing into the particulate filter 22 becomes rich, NO is
released from the active oxygen release agent/NO.sub.x absorbent
61. This NO is reduced by the unburned hydrocarbons and CO and
therefore no NO is discharged into the atmosphere at this time as
well. Further, the particulates deposited on the particulate filter
22 are removed by oxidation by the active oxygen released from the
active oxygen release agent/NO.sub.x absorbent 61.
[0107] As already explained with reference to FIG. 6, the action of
release of active oxygen from the active oxygen release agent 61 is
started from when the temperature of the particulate filter 22 is
considerably low. The same is true even when using the active
oxygen release agent/NO.sub.x absorbent 61. As opposed to this, the
action of absorption of NO.sub.x in the active oxygen release
agent/NO.sub.x absorbent 61 does not start unless the temperature
TF of the particulate filter 22 becomes higher than the temperature
of start of release of active oxygen. This is considered to be
because the release of active oxygen is caused if oxygen is robbed
from the potassium nitrate KNO.sub.3 for example, while the action
of absorption of NO.sub.x is not started unless the platinum Pt is
activated.
[0108] FIG. 11 shows the amount G of the particulates removable by
oxidation and the NO.sub.x absorption rate when using potassium K
as the active oxygen release agent/NO.sub.x absorbent 61. From FIG.
11, it is learned that the action of release of active oxygen is
started when the temperature TF of the particulate filter 22 is
less than 200.degree. C., while the action of absorption of
NO.sub.x is not started unless the temperature TF of the
particulate filter 22 is over 200.degree. C.
[0109] On the other hand, the action of release of active oxygen
becomes more active the higher the temperature TF of the
particulate filter 22. As opposed to this, the action of absorption
of NO.sub.x disappears when the temperature TF of the particulate
filter 22 becomes higher. That is, if the temperature TF of the
particulate filter 22 exceeds a certain temperature, in the example
shown in FIG. 11, about 500.degree. C., the nitrate ions
NO.sub.3.sup.- or potassium nitrate KNO.sub.3 break down under heat
and NO is released from the active oxygen release agent/NO.sub.x
absorbent 61. In this state, the amount of release of NO becomes
greater than the amount of absorption of NO.sub.x and therefore, as
shown in FIG. 11, the NO.sub.x absorption rate falls.
[0110] FIG. 11 shows the NO.sub.x absorption rate when using
potassium K as the NO.sub.x absorbent or the active oxygen release
agent/NO.sub.x absorbent 61. In this case, the temperature range of
the particulate filter 22 where the NO.sub.x absorption rate
becomes higher differs by the metal used. For example, when using
barium Ba as the NO.sub.x absorbent or the active oxygen release
agent/NO.sub.x absorbent 61, the temperature range of the
particulate filter 22 where the NO.sub.x absorption rate becomes
higher becomes narrower than the case of use of potassium K shown
in FIG. 11.
[0111] As explained above, however, to enable the particulates in
the exhaust gas to be removed by oxidation without depositing in
layers on the particulate filter 22, it is necessary to make the
amount M of discharged particulates smaller than the amount G of
the particulates removable by oxidation. If just making the amount
M of discharged particulates smaller than the amount G of the
particulates removable by oxidation, however, the action of
absorption of NO.sub.x by the NO.sub.x absorbent or the active
oxygen release agent/NO.sub.x absorbent 61 does not occur. To
ensure the action of absorption of NO.sub.x by the NO.sub.x
absorbent or the active oxygen release agent/NO.sub.x absorbent, it
is necessary to maintain the temperature TF of the particulate
filter 22 within the temperature range where the action of
absorption of NO.sub.x occurs. In this case, the temperature range
of the particulate filter 22 where the NO.sub.x absorption action
occurs has to be made a temperature range where the NO.sub.x
absorption rate becomes more than a certain value, for example,
more than 50 percent. Therefore, when using potassium K as the
NO.sub.x absorbent or the active oxygen release agent/NO.sub.x
absorbent 61, as will be understood from FIG. 11, the temperature
TF of the particulate filter 22 has to be maintained between about
250.degree. C. to 500.degree. C.
[0112] Therefore, in this embodiment of the present invention, to
remove by oxidation the particulates in the exhaust gas without
they depositing in layers on the particulate filter 22 and to
absorb the NO.sub.x in the exhaust gas, the amount M of discharged
particulates is maintained smaller than the amount G of the
particulates removable by oxidation continuously and temperature TF
of the particulate filter 22 is maintained in the temperature range
where the NO.sub.x absorption rate of the particulate filter 22
becomes more than a certain value. That is, the amount X of
discharged particulates and the temperature TF of the particulate
filter 22 are kept in the simultaneous particulates and NO.sub.x
treatment region shown by the hatching in FIG. 11.
[0113] Even if the amount M of discharged particulates and the
temperature of the particulate filter 22 are maintained in the
simultaneously particulate and NO.sub.x treatment region in this
way, sometimes the amount M of discharged particulates and the
temperature of the particulate filter 22 will move outside the
simultaneous particulate and NO.sub.x treatment region. In this
case, in this embodiment of the present invention, at least one of
the amount M of discharged particulates, amount G of the
particulates removable by oxidation, and temperature TF of the
particulate filter 22 is controlled so that the amount M of
discharged particulates and the temperature of the particulate
filter 22 move inside the simultaneous particulate and NO.sub.x
treatment region. This will be explained next with reference to
FIG. 12.
[0114] First, the case when the amount M of discharged particulates
and the temperature of the particulate filter 22 reach the point A
outside the simultaneous particulate and NO.sub.x treatment region
shown in FIG. 12, that is, the amount M of discharged particulates
becomes larger than the amount G of the particulates removable by
oxidation and the temperature TF of the particulate filter 22
becomes lower than the lower limit temperature of the simultaneous
particulate and NO.sub.x treatment region, will be explained. In
this case, as shown by the arrow, by raising the temperature TF of
the particulate filter 22, the amount M of discharged particulates
and the temperature TF of the particulate filter 22 are returned to
within the simultaneous particulate and NO.sub.x treatment
region.
[0115] Next, the case where the amount M of discharged particulates
and the temperature TF of the particulate filter 22 reach the point
B outside the simultaneous particulate and NO.sub.x treatment
region shown in FIG. 12, that is, where the amount M of discharged
particulates becomes greater than the amount G of the particulates
removable by oxidation and the temperature TF of the particulate
filter 22 is inside the temperature range of the simultaneous
particulate and NO.sub.x treatment region will be explained. In
this case, as shown by the arrow, the amount M of discharged
particulates is reduced to return the amount M of discharged
particulates and the temperature TF of the particulate filter 22 to
the simultaneous particulate and NO.sub.x treatment region.
[0116] Next, the case where the amount M of discharged particulates
and the temperature TF of the particulate filter 22 reach the point
C outside the simultaneous particulate and NO.sub.x treatment
region shown in FIG. 12, that is, where the amount M of discharged
particulates becomes larger than the amount G of the particulates
removable by oxidation and the temperature TF of the particulate
filter 22 becomes higher than the upper limit temperature of the
simultaneous particulate and NO.sub.x treatment region, will be
explained. In this case, as shown by the arrow, the amount M of
discharged particulates is reduced and the temperature TF of the
particulate filter 22 is reduced so as to return the amount M of
discharged particulates and the temperature TF of the particulate
filter 22 to the simultaneous particulate and NO.sub.x treatment
region.
[0117] In this way, by reducing the amount M of discharged
particulates or raising or reducing the temperature TF of the
particulate filter 22 when the amount X of discharged particulates
and the temperature of the particulate filter 22 become outside the
simultaneous particulates and NO.sub.x treatment region, the amount
M of discharged particulate and the temperature of the particulate
filter 22 are returned inside the simultaneous particulate and
NO.sub.x treatment region. Note that, as another method, it is also
possible to return the amount M of discharged particulates and the
temperature of the particulate filter 22 to the inside of the
simultaneous particulate and NO.sub.x treatment region by
increasing the amount G of the particulates removable by oxidation.
Therefore, next, an explanation will be given of the method of
reducing the amount M of discharged particulates, the method of
raising or lowering the temperature TF of the particulate filter
22, and the method of increasing the amount G of the particulates
removable by oxidation.
[0118] Next, an explanation will be given of the method of using
low temperature combustion to control the amount M of discharged
particulates and the temperature TF of the particulate filter
22.
[0119] In the engine shown in FIG. 1, if the EGR rate (amount of
EGR gas/(amount of EGR gas+amount of intake air)) is increased, the
amount of smoke generated gradually increases and peaks. If the EGR
rate is further raised, the amount of generation of smoke then
rapidly falls. This will be explained with reference to FIG. 13
showing the relation between the EGR rate and the smoke when
changing the degree of cooling of the EGR gas. Note that, in FIG.
13, the curve A shows the case of forced cooling of the EGR gas to
maintain the temperature of the EGR gas at about 90.degree. C.,
curve B shows the case of cooling the EGR gas by a small sized
cooling device, and curve C shows the case of not force cooling the
EGR gas.
[0120] As shown by curve A of FIG. 13, when force cooling the EGR
gas, the amount of generation of smoke peaks when the EGR rate is
slightly lower than 50 percent. In this case, if the EGR rate is
made more than about 55 percent, almost no smoke is generated any
longer. On the other hand, as shown by curve B of FIG. 13, when
slightly cooling the EGR gas, the amount of generation of smoke
peaks when the EGR rate becomes slightly higher than 50 percent. In
this case, if the EGR rate is made more than about 65 percent,
almost no smoke is generated any longer. Further, as shown by curve
C in FIG. 13, when the EGR gas is not force cooled, the amount of
generation of smoke peaks near an EGR rate of 55 percent. In this
case, almost no smoke is generated any longer when the EGR rate is
over about 70 percent.
[0121] The reason why smoke is no longer generated when the EGR gas
rate is made over 55 percent is that due to the heat absorbing
action of the EGR gas, the gas temperature of the fuel and its
surroundings at the time of combustion does not become that high,
that is, low temperature combustion is performed, and as a result
the hydrocarbon does not grow into soot.
[0122] This low temperature combustion has the characteristic of
enabling suppression of the generation of smoke and reduction of
the amount of generation of NO.sub.x regardless of the air-fuel
ratio. That is, when the air-fuel ratio is made rich, the fuel
becomes excessive, but since the combustion temperature is
suppressed to a low temperature, the excess fuel does not grow to
soot and therefore no smoke is generated. Further, at this time,
only an extremely small amount of NO.sub.x is produced. On the
other hand, when the mean air-fuel ratio is lean or the air-fuel
ratio is the stoichiometric air-fuel ratio, if the combustion
temperature becomes high, a small amount of soot is produced, but
under low temperature combustion, the combustion temperature is
suppressed to a low temperature, so no smoke is generated at all
and only an extremely small amount of NO.sub.x is generated.
[0123] On the other hand, if low temperature combustion is
performed, the gas temperature of the fuel and its surroundings
becomes low, but the temperature of the exhaust gas rises. This
will be explained with reference to FIGS. 14A and 14B.
[0124] The solid line of FIG. 14A shows the relationship between
the mean gas temperature Tg in the combustion chamber 5 and the
crank angle when low temperature combustion is performed, while the
broken line of FIG. 14A shows the relationship between the mean gas
temperature Tg in the combustion chamber 5 and the crank angle when
normal combustion is performed. Further, the solid line of FIG. 14B
shows the relationship between the gas temperature of the fuel and
its surroundings when low temperature combustion is performed,
while the broken line of FIG. 14B shows the relationship between
the gas temperature Tf of the fuel and its surroundings and the
crank angle when normal combustion is performed.
[0125] When low temperature combustion is performed, the amount of
EGR gas becomes larger than when normal combustion is performed.
Therefore, as shown in FIG. 14A, before top dead center of the
compression stroke, that is, during the compression stroke, the
mean gas temperature Tg at the time of low temperature combustion
shown by the solid line becomes higher than the mean gas
temperature Tg at the time of normal combustion shown by the broken
line. Note that at this time, as shown in FIG. 14B, the gas
temperature Tf of the fuel and its surroundings becomes about the
same temperature as the mean gas temperature Tg.
[0126] Next, the combustion starts near top dead center of the
compression stroke. In this case, at the time of low temperature
combustion, as shown by the solid line of FIG. 14B, due to the heat
absorbing action of the EGR gas, the gas temperature Tf of the fuel
and its surroundings does not become that high. As opposed to this,
at the time of normal combustion, there is a large amount of oxygen
around the fuel, as shown by the broken line of FIG. 14B, the gas
temperature Tf of the fuel and its surroundings becomes extremely
high. When normal combustion is performed in this way, the gas
temperature Tf of the fuel and its surroundings becomes
considerably high compared with the case of low temperature
combustion, but the temperature of the gas other than the majority
becomes lower when normal combustion is performed compared with
when low temperature combustion is performed. Therefore, as shown
in FIG. 14A, the mean gas temperature Tg in the combustion chamber
5 near top dead center of the compression stroke becomes higher at
the time of low temperature combustion compared with normal
combustion. As a result, as shown in FIG. 14A, the temperature of
the already burned gas in the combustion chamber 5 after the
combustion is finished becomes higher at the time of low
temperature combustion compared with normal combustion. Therefore,
at the time of low temperature combustion, the temperature of the
exhaust gas becomes high.
[0127] If low temperature combustion is performed in this way, the
amount of generation of smoke, that is, the amount M of discharged
particulate, becomes smaller and the temperature of the exhaust gas
rises. Therefore, when switching from normal combustion to low
temperature combustion during engine operation, the amount M of
discharged particulate can be reduced and the temperature TF of the
particulate filter 22 can be raised. AS opposed to this, when
switching from low temperature combustion to normal combustion, the
temperature TF of the particulate filter 22 falls. At this time,
however, the amount M of discharged particulates increases.
Whatever the case, by switching between normal combustion and low
temperature combustion, the amount M of discharged particulates and
the temperature of the particulate filter 22 can be controlled.
[0128] If the required torque TQ of the engine becomes higher,
however, that is, if the amount of fuel injection becomes greater,
the gas temperature of the fuel and its surroundings at the time of
combustion becomes higher, so low temperature combustion becomes
difficult. That is, low temperature combustion becomes possible
only at the time of engine medium and low load operation where the
amount of generation of heat by the combustion is relatively small.
In FIG. 15, region I shows the operating region where first
combustion where there is a larger amount of inert gas in the
combustion chamber 5 than the amount of inert gas where the
generation of soot peaks, that is, low temperature combustion, can
be performed, while region II shows the operating region where
second combustion where there is a smaller amount of inert gas in
the combustion chamber 5 than the amount of inert gas where the
generation of soot peaks, that is, normal temperature combustion,
can be performed.
[0129] FIG. 16 shows the target air-fuel ratio A/F in the case of
low temperature combustion in the operating region I, while FIG. 17
shows the opening degree of the throttle valve 17, the opening
degree of the EGR control valve 25, the EGR rate, the air-fuel
ratio, the injection start timing .theta.S, the injection end
timing .theta.E, and the amount of injection in accordance with the
required torque TQ at the time of low temperature combustion in
operating region I. Note that FIG. 17 also shows the opening degree
of the throttle valve 17 at the time of normal combustion performed
in operating region II.
[0130] From FIG. 16 and FIG. 17, it is understood that when low
temperature combustion is performed in operating region I, the EGR
rate is made over 55 percent and the air-fuel ratio A/F is made a
lean air-fuel ratio of 15.5 to about 18. Note that as explained
above, when low temperature combustion is performed in operating
region I, even if the air-fuel ratio is made rich, almost no smoke
is produced.
[0131] Next, an explanation will be given of the method for
increasing the concentration of oxygen in the exhaust gas for
increasing the amount G of the particulates removable by oxidation.
If the concentration of oxygen in the exhaust gas increases, the
amount of oxygen absorbed in the active oxygen release agent 61
increases, so the amount of active oxygen released from the active
oxygen release agent 61 increases and therefore the amount G of the
particulates removable by oxidation increases.
[0132] As a method for executing this method, the method of
controlling the EGR rate may be mentioned. That is, when the amount
G of the particulates removable by oxidation is to be increased,
the opening degree of the EGR control valve 25 is reduced so that
the EGR rate falls. The fall in the EGR rate means that the ratio
of the amount of intake air in the intake air increases. Therefore,
if the EGR rate falls, the concentration of oxygen in the exhaust
gas rises. As a result, the amount M of discharged particulates
increases. Further, if the EGR rate falls, as mentioned above, the
amount M of discharged particulates falls. Therefore, if the EGR
rate falls, the amount M of discharged particulates rapidly becomes
smaller than the amount G of the particulates removable by
oxidation.
[0133] Now, as explained above, when the air-fuel ratio of the
exhaust gas is lean, the NO.sub.x in the exhaust gas is absorbed in
the active oxygen release agent/NO.sub.x absorbent 61. However,
there are limits to the NO.sub.x absorption capability of the
NO.sub.x absorbent 61. It is necessary to cause the release of
NO.sub.x from the active oxygen release agent/NO.sub.x absorbent 61
before the NO.sub.x absorption capability of the active oxygen
release agent/NO.sub.x absorbent 61 becomes saturated. Therefore,
it is necessary to estimate the amount of NO.sub.x absorbed in the
active oxygen release agent/NO.sub.x absorbent 61. Therefore, in
this embodiment of the present invention, the NO.sub.x absorption
amount A per unit time is set, in advance, in the form of a map
shown in FIG. 18 as a function of the required torque TQ and engine
speed N. By cumulatively adding the NO.sub.x absorption amount A
per unit time, the NO.sub.x amount .SIGMA.NOX absorbed in the
active oxygen release agent/NO.sub.x absorbent 61 may be
estimated.
[0134] Further, in this embodiment of the present invention, when
the NO.sub.x absorption amount .SIGMA.NOX exceeds a predetermined
allowable maximum value MAXN, the air-fuel ratio of the exhaust gas
flowing into the active oxygen release agent/NO.sub.x absorbent 61
is made temporarily rich. Due to this, NO.sub.x is made to be
released from the active oxygen release agent/NO.sub.x absorbent
61.
[0135] The exhaust gas, however, contains SO.sub.x. The active
oxygen release agent/NO.sub.x absorbent 61 absorbs not only the
NO.sub.x, but also the SO.sub.x. The mechanism of absorption of
SO.sub.x in the active oxygen release agent/NO.sub.x absorbent 61
is the same as the mechanism of absorption of the NO.sub.x.
[0136] That is, explaining this taking as an example the case of
carrying platinum Pt and potassium K on the carrier in the same way
as explained with respect to the mechanism of absorption of
NO.sub.x, as explained above, the oxygen O.sub.2 adheres to the
surface of the platinum Pt in the form of O.sub.2.sup.- or O.sup.2-
when the air-fuel ratio of the exhaust gas is lean. The SO.sub.2 in
the exhaust gas reacts with the O.sub.2.sup.- or O.sup.2- on the
surface of the platinum Pt to become SO.sub.3. Next, part of the
SO.sub.3 which is produced is absorbed in the active oxygen release
agent 61 while being oxidized on the platinum Pt and diffuses in
the active oxygen release agent/NO.sub.x absorbent 61 in the form
of sulfate ions SO.sub.4.sup.2- while bonding with the potassium Pt
to produce potassium sulfate K.sub.2SO.sub.4.
[0137] This sulfate, K.sub.2SO.sub.4, is stable and hard to break
down. As explained above, even if the air-fuel ratio of the exhaust
gas is made rich for releasing the NO.sub.x from the active oxygen
release agent/NO.sub.x absorbent 61, the sulfate K.sub.2SO.sub.4
remains as it is without breaking down. Therefore, the sulfate
K.sub.2SO.sub.4 increases in the active oxygen release
agent/NO.sub.x absorbent 61 with time. Accordingly, the amount of
NO.sub.x which the active oxygen release agent/NO.sub.x absorbent
61 can absorb falls with time.
[0138] The sulfate K.sub.2SO.sub.4 breaks down when the temperature
of the active oxygen release agent/NO.sub.x absorbent 61 exceeds a
certain temperature determined by the active oxygen release
agent/NO.sub.x absorbent 61, for example, about 600.degree. C. At
this time, if the air-fuel ratio of the exhaust gas flowing into
the active oxygen release agent/NO.sub.x absorbent 61 is made rich,
the SO.sub.x is released from the active oxygen release
agent/NO.sub.x absorbent 61. Release of the SO.sub.x from the
active oxygen release agent/NO.sub.x absorbent 61, however, takes a
considerably long time compared with release of NO.sub.x from the
active oxygen release agent/NO.sub.x absorbent 61.
[0139] Therefore, in this embodiment of the present invention, when
SO.sub.x is to be released from the active oxygen release
agent/NO.sub.x absorbent 61, the temperature of the active oxygen
release agent/NO.sub.x absorbent 61 is raised to about 600.degree.
C. while maintaining the state where the air-fuel ratio is lean and
the amount M of discharged particulates is smaller than the amount
G of the particulates removable by oxidation, then SO.sub.x is made
to be released from the active oxygen release agent/NO.sub.x
absorbent 61 while the air-fuel ratio of the exhaust gas flowing to
the active oxygen release agent/NO.sub.x absorbent 61 is
alternately switched between rich and lean.
[0140] Further, when the temperature TF of the active oxygen
release agent/NO.sub.x absorbent 61 is raised to about 600.degree.
C., the state is maintained where the air-fuel ratio is lean and
the amount M of discharged particulates is smaller than the amount
G of the particulates removable by oxidation. Therefore, at this
time, even if the particulates deposit on the particulate filter
22, the deposited particulates are removed by oxidation while the
temperature TF of the active oxygen release agent/NO.sub.x
absorbent 61 is raised to about 600.degree. C.
[0141] On the other hand, there are various methods for making the
air-fuel ratio of the exhaust gas flowing into the active oxygen
release agent/NO.sub.x absorbent 61 rich to release the NO.sub.x or
SO.sub.x from the active oxygen release agent/NO.sub.x absorbent
61. For example, when performing low temperature combustion, by
making the air-fuel ratio in the combustion chamber 5 rich during
low temperature combustion, it is possible to make the air-fuel
ratio of the exhaust gas flowing into the active oxygen release
agent/NO.sub.x absorbent 61 rich.
[0142] Further, as explained above, when the air-fuel ratio of the
exhaust gas is made rich, the active oxygen is released all at once
from the active oxygen release agent/NO.sub.x absorbent 61. Due to
this, the particulates deposited on the particulate filter 22 are
rapidly oxidized. Even after this, however, if the air-fuel ratio
of the exhaust gas continues to be made rich, oxygen is not stored
in the active oxygen release agent/NO.sub.x absorbent 61. Further,
there is almost no oxygen present in the exhaust gas. Therefore,
the particulates are deposited in layers on the particulate filter
22 without being oxidized.
[0143] Therefore, in this embodiment of the present invention, when
releasing SO.sub.x, which requires that the air-fuel ratio be made
rich for a long period, the air-fuel ratio of the exhaust gas
flowing into the active oxygen release agent/NO.sub.x absorbent 61
is alternately switched between rich and lean as explained above.
By doing this, when the air-fuel ratio of the exhaust gas becomes
lean, the particulates on the particulate filter 22 are removed by
oxidation by the active oxygen in the exhaust gas or the active
oxygen released from the active oxygen release agent/NO.sub.x
absorbent 61. Therefore, it is possible to prevent the particulates
from depositing in layers on the particulate filter 22.
[0144] Next, an explanation will be made, with reference to FIG.
26, of the processing routine of the NO.sub.x releasing flag set
when the NO.sub.x is to be released from the active oxygen release
agent/NO.sub.x absorbent 61 and the SO.sub.x releasing flag set
when the SO.sub.x is to be released from the active oxygen release
agent/NO.sub.x absorbent 61. Note that this routine is executed by
interruption every certain time interval.
[0145] With reference to FIG. 19, first, at step 100, the NO.sub.x
absorption amount A per unit time is calculated from the map shown
in FIG. 18. Next, at step 101, A is added to the NO.sub.x
absorption amount .SIGMA.NOX. Next, at step 102, it is decided if
the NO.sub.x absorption amount .SIGMA.NOX has exceeded the
allowable maximum value MAXN. When .SIGMA.NOX>MAXN, the routine
proceeds to step 103, the NO.sub.x releasing flag showing that the
NO.sub.x is to be released is set. Next, the routine proceeds to
step 104.
[0146] At step 104, the product k Q of the constant k multiplied
with the injection amount Q is added to .SIGMA.SOX. The fuel
contains a certain amount of sulfur S. Therefore, the amount of
SO.sub.x absorbed in the active oxygen release agent/NO.sub.x
absorbent 61 can be expressed by k Q. Therefore, the .SIGMA.SOX
obtained by successively adding k Q expresses the amount of
SO.sub.x estimated to be absorbed in the active oxygen release
agent/NO.sub.x absorbent 61. At step 105, it is decided if the
SO.sub.x amount .SIGMA.SOX is over the allowable maximum MAXs. When
.SIGMA.SOX>MAXS, the routine proceeds to step 106, where the
SO.sub.x releasing flag is set.
[0147] Next, an explanation will be made of the control of the
operation while referring to FIG. 27 and FIG. 28.
[0148] Referring to FIG. 20 and FIG. 21, first, at step 200, it is
decided if the SO. releasing flag is set. When the SO.sub.x
releasing flag is not set, the routine proceeds to step 201, where
it is decided if the temperature TF of the particulate filter 22 is
lower than the lower limit temperature T.sub.min of the
simultaneous particulate and NO.sub.x treatment region shown by the
hatching in FIG. 11, for example, 250.degree. C. When
TF<T.sub.min, the routine proceeds to step 202, where one of the
methods for raising the temperature TF of the particulate filter 22
is executed. Next, the routine proceeds to step 207.
[0149] On the other hand, when it is decided at step 201 that
TF.gtoreq.T.sub.min, the routine proceeds to step 203, where it is
decided if the temperature TF of the particulate filter 22 is
higher than the upper limit temperature T.sub.max of the
simultaneous particulate and NO.sub.x treatment region shown by the
hatching in FIG. 11, for example 500.degree. C. When
TF>T.sub.max, the routine proceeds to step 204, where one of the
methods for reducing the temperature TF of the particulate filter
22 is executed. Next, the routine proceeds to step 207.
[0150] On the other hand, when it is decided at step 203 that
TF.ltoreq.T.sub.max, the routine proceeds to step 205, where it is
decided if the amount M of discharged particulates is larger than
amount G of the particulates removable by oxidation. When M>G,
the routine proceeds to step 206, where one of the methods for
reducing the amount M of discharged particulate or one of the
methods for increasing the amount G of the particulates removable
by oxidation is executed. Next, the routine proceeds to step
207.
[0151] On the other hand, when it is decided at step 205 that MEG,
the routine proceeds to step 207. At step 207, it is decided if the
NO.sub.x flag has been set. When the NO.sub.x releasing flag has
been set, the routine proceeds to step 208, where the opening
degree of the throttle valve 17 is controlled, then at step 209,
the opening degree of the EGR control valve 25 is controlled. Next,
at step 210, the fuel injection is controlled.
[0152] As opposed to this, when it is judged at step 207 that the
NO.sub.x releasing flag has been set, the routine proceeds to step
211, where the opening degree of the throttle valve 17 is
controlled. Next, at step 212, the opening degree of the EGR
control valve 25 is controlled. Next, at step 213, one of the
methods for making the air-fuel ratio of the exhaust gas
temporarily rich is executed to release the NO.sub.x and the
NO.sub.x releasing flag is reset.
[0153] On the other hand, when it is decided at step 200 that the
SO.sub.x releasing flag has been set, the routine proceeds to step
214, where it is decided if the temperature TF of the particulate
filter 22 is more than the temperature where SO.sub.x can be
released, for example, 600.degree. C. When TF.ltoreq.600.degree.
C., the routine proceeds to step 215, the opening degree of the
throttle valve 17 is controlled, then at step 216, the opening
degree of the EGR control valve 25 is controlled.
[0154] Next, at step 217, it is decided if the amount M of
discharged particulates is larger than the amount G of the
particulates removable by oxidation. When M>G, the routine
proceeds to step 218, where one of the methods for reducing the
amount M of discharged particulates or one of the methods for
increasing the amount G of the particulates removable by oxidation
is executed. Next, at step 219, one of the methods for raising the
temperature TF of the particulate filter 22 to about 600.degree. C.
is executed.
[0155] On the other hand, when it is decided at step 214 that
TF>600.degree. C., the routine proceeds to step 220, where the
opening degree of the throttle valve 17 is controlled and then, at
step 221, the opening degree of the EGR control valve 25 is
controlled. Next, at step 222, by alternately switching the
air-fuel ratio of the exhaust gas between rich and lean, the
release of SO.sub.x is controlled to release the SO.sub.x from the
active oxygen release agent/NO.sub.x absorbent 61.
[0156] Next, at step 223, the SO.sub.x release amount
.DELTA.SO.sub.x is subtracted from the SO.sub.x amount .SIGMA.SOX.
This SO.sub.x release amount .DELTA.SO.sub.x may be made a certain
value or may be changed in accordance with the engine operating
state. Next, at step 224, it is decided if the SO.sub.x amount
.SIGMA.SOX has become negative. When .SIGMA.SOX<0, the routine
proceeds to step 225, where the NO.sub.x releasing flag and the
SO.sub.x releasing flag are reset.
[0157] Generally speaking, however, in an internal combustion
engine, at the time of engine low load operation, the temperature
of the exhaust gas is low. Therefore, sometimes it is difficult to
make the amount G of the particulates removable by oxidation larger
than the amount M of discharged particulates. If low temperature
combustion is performed as mentioned above, however, the amount M
of discharged particulates is extremely small. Further, since the
temperature of the exhaust gas is high, the temperature TF of the
particulate filter 22 becomes high. Therefore, even during engine
low load operation, it is possible to easily increase the amount M
of discharged particulates from the amount M of discharged
particulates. Therefore, low temperature combustion can be said to
be extremely suited to the exhaust gas purification apparatus of
the present invention.
[0158] As explained above, however, this low temperature combustion
is only performed in the low side operating region I shown in FIG.
15 and is not performed in the high load side operating region II.
Therefore, even when performing low temperature combustion, low
temperature combustion is performed only when the engine operating
state is in the operating region I of FIG. 15. When the engine
operating state exceeds the boundary X(N) and shifts to the
operating region II, low temperature combustion is switched to
normal combustion. That is, temperature combustion is performed in
operating region I, while normal combustion is performed in
operating region II.
[0159] Referring to FIGS. 22-25, an explanation will be given of a
bypass mechanism of this embodiment. The exhaust pipe 20a is
connected to an exhaust flow change pipe 80. The exhaust flow
change pipe 80 has three openings. These openings are connected to
a first exhaust branch pipe 81a, a second exhaust branch pipe 81b,
and an exhaust pipe 82, respectively.
[0160] That is, in the exhaust flow change pipe 80, the first and
second exhaust branch pipes 81a, 81b of the pair branch from the
exhaust pipe 20a. The first exhaust branch pipe 81a is connected to
one end of the particulate filter 22. On the other hand, the second
exhaust branch pipe 81b is connected to the other end of the
particulate filter 22. That is, the first and second exhaust branch
pipes 81a, 81b are connected to each other to make a loop-shaped
exhaust passage.
[0161] The particulate filter 22 is arranged in the loop-shaped
exhaust passage. Below, for the sake of convenience in the
explanation, the end of the particulate filter 22 connected to the
first exhaust branch pipe 81a is referred to as a first end, and
the end of the particulate filter 22 connected to the second
exhaust branch pipe 81b is referred to as a second end.
[0162] A switching valve 80a is arranged in the exhaust flow change
pipe 80. By changing the rotation position of the switching valve
80a, the in flowing manner of the exhaust gas is changed between
the in flowing manner of the exhaust gas into the first end of the
particulate filter 22 through the first exhaust branch pipe 81a,
the in flowing manner of the exhaust gas into the second end of the
particulate filter 22 through the second exhaust branch pipe 81b,
and the inflowing manner of the exhaust gas directly into the
exhaust pipe 82 without passing through the particulate filter
22.
[0163] When the switching valve 80a is positioned at a first
rotation position as shown in FIG. 22, the exhaust gas upstream of
the exhaust flow change pipe 80 flows into the particulate filter
22 at the first end thereof through the first exhaust branch pipe
81a as shown by an arrow of FIG. 22. The exhaust gas flowing into
the particulate filter 22 at the first end thereof flows out from
the particulate filter 22 at the second end thereof to the exhaust
pipe 82 downstream of the exhaust flow change pipe 80 through the
second exhaust branch pipe 81b.
[0164] Further, when the switching valve 80a is positioned at the
second rotation position as shown in FIG. 24, the exhaust gas
upstream of the exhaust flow change pipe 80 flows into the
particulate filter 22 at the second end thereof through the second
exhaust branch pipe 81b. The exhaust gas flowing into the
particulate filter 22 at the second end thereof flows out from the
particulate filter 22 at the first end thereof to the exhaust pipe
82 downstream of the exhaust flow switching valve 80 through the
first exhaust branch pipe 81a.
[0165] In this embodiment, as explained in detail in the below, the
rotation position of the switching valve 80a is changed
alternatively between the first and second rotation positions each
time a predetermined period has elapsed to change the direction of
the inflow of the exhaust gas into the particulate filter 22.
Therefore, the particulates flow in the particulate filter 22 or
the partitions 54 thereof so that the particulates are removed by
oxidation.
[0166] When the switching valve 80a is positioned at a neutral
position just intermediate between the first and second rotation
positions as shown in FIG. 25, the exhaust gas upstream of the
exhaust flow change pipe 80 flows directly into the exhaust pipe 80
downstream of the exhaust flow change pipe 80 without passing the
particulate filter 22 as shown by an arrow in FIG. 25.
[0167] At the neutral position, the pressure of the exhaust gas at
the first end of the particulate filter 22 is generally equal to
that at the second end of the particulate filter 22, so almost of
the exhaust gas does not flow into the particulate filter 22.
Therefore, the exhaust gas is made to bypass the particulate filter
22, so the amount of the exhaust gas flowing into the particulate
filter 22 generally becomes zero.
[0168] Even if the particulates are removed by oxidation in the
particulate filter 22 by using an exhaust gas purification method
as explained above, the particulates are sometimes deposited on the
surface of the particulate filter 22. If the particulate deposited
on the surface of the particulate filter 22 remains as it is, the
deposited particulates cover the surface of the particulate filter
22, and thus the exhaust gas may not pass through the particulate
filter 22.
[0169] Therefore, in this embodiment, when the amount of the
particulates deposited on the surface of the particulate filter 22
becomes larger than a predetermined amount, the deposited
particulates are forcibly oxidized or gradually burned to remove
the particulates from the particulate filter 22. It is possible to
oxidize or gradually burn the deposited particulates by raising the
temperature of the particulate filter 22 to a certain temperature
(For example, a temperature at which the particulates are
oxidized.).
[0170] For example, it is possible to raise the temperature of the
particulate filter 22 by feeding oxygen and hydrocarbon to the
particulate filter 22 and then burning the oxygen and hydrocarbon
in the particulate filter 22.
[0171] Further, when the engine performs the low temperature
combustion, exhaust gas having a high temperature is discharged
from the engine, so it is also possible to raise the temperature of
the particulate filter 22 by performing low temperature
combustion.
[0172] In this embodiment, when the amount of the deposited
particulates becomes relatively large, a temperature raising
process to raise the temperature of the particulate filter 22 to a
certain temperature, such as the particulate oxidizing temperature,
is performed to forcibly oxidize or gradually burn the deposited
particulates.
[0173] However, during the temperature raising process, the
deposited particulates may possibly burn all at once. Further,
without performing the temperature raising process, when the
temperature of the particulate filter 22 exceeds a temperature at
which the particulates are ignited and burn all at once with
emitting a luminous flame, the deposited particulates may burn all
at once. In this case, the temperature of the particulate filter 22
rises rapidly.
[0174] Therefore, a part of the particulate filter 22 may possibly
be melted, and thermally damaged by the heat of the burning of the
particulates. Otherwise, the active oxygen release agent carried on
the particulate filter 22 may possibly be deteriorated by the heat
of the burning of the particulates. To prevent the melting of the
particulate filter 22 or deterioration of the active oxygen release
agent, it is preferable to prevent the deposited particulates from
burning.
[0175] If the deposited particulates do not burn, however, the
amount of the deposited particulates gradually becomes large, so
the action of oxidizing the particulates in the particulate filter
22 is suppressed. Consequently, the particulate filter cannot
remove the particulates by oxidation. Further, if the fine holes of
the partitions 54 of the particulate filter 22 are clogged by the
deposited particulates, the exhaust gas cannot pass the particulate
filter 22.
[0176] In this embodiment, it is judged if the particulate filter
22 will be thermally deteriorated. When it is judged that the
particulate filter 22 will be thermally deteriorated, the rotation
position of the switching valve 80a is set at the neutral position
so that the exhaust gas is made to bypass the particulate filter
22. In this way, oxygen is not fed to the particulate filter 22, so
the deposited particulates do not burn.
[0177] On the other hand, when it is judged that the particulate
filter 22 will not be thermally deteriorated, the rotation position
of the switching valve 80a is set at the first or second position
so that the exhaust gas flows into the particulate filter 22. In
this way, oxygen is fed to the particulate filter 22, so the
deposited particulates are forcibly oxidized or gradually burn.
[0178] An explanation will be given of a method for judging if the
particulate filter will be thermally deteriorated according to this
embodiment. Commonly, the larger the amount of the deposited
particulates, the larger the amount of the heat produced by the
deposited particulates burning all at once. Therefore, when the
amount of the deposited particulates is large, the possibility that
the particulate filter 22 is thermally deteriorated is high. That
is, it is possible to judge if the particulate filter 22 will be
thermally deteriorated on the basis of the amount of the deposited
particulates.
[0179] It has been considered that the amount of the deposited
particulates can be estimated on the basis of the difference
(pressure loss) in the pressures of the exhaust gas upstream and
downstream of the particulate filter 22. According to the recent
research, it has been found that, even if the pressure loss is
small, the amount of the deposited particulates is sometimes
large.
[0180] This is because the particulates PM are deposited on the
partitions 54 as shown in FIG. 26, so the deposited particulates do
not close inlets of the fine holes of the partitions 54. Mainly,
two things, that is, the large amount of heat produced by the
deposited particulates burning and the small amount of heat
radiated from the particulate filter 22 are deemed to cause the
thermal deterioration of the particulate filter 22.
[0181] The larger the amount of oxygen flowing into the particulate
filter 22, the larger the amount of heat produced by the burning of
the deposited particulates. Further, the smaller the amount of the
exhaust gas flowing into the particulate filter 22, the smaller the
amount of heat radiated from the particulate filter 22.
[0182] In this embodiment, when the amount of oxygen flowing into
the particulate filter 22 is large or the amount of the exhaust gas
flowing into the particulate filter 22 is small under the condition
that the temperature of the particulate filter 22 is higher than
the particulate ignition temperature, it is judged that the
particulate filter 22 will be thermally deteriorated.
[0183] On the other hand, when the amount of oxygen flowing into
the particulate filter 22 is small or the amount of the exhaust gas
flowing into the particulate filter 22 is large even under the
condition that the temperature of the particulate filter 22 is
higher than the particulate ignition temperature, it is judged that
the particulate filter 22 will not be thermally deteriorated.
[0184] In this way, if the possibility of the thermal deterioration
of the particulate filter 22 is considered, the deposited
particulates can be removed from the particulate filter 22 without
thermally deteriorating the particulate filter 22.
[0185] An explanation will be given in detail of a process for
controlling the switching valve, including the above explained
processes for preventing the thermal deterioration of the
particulate filter and oxidizing the deposited particulates,
referring to FIGS. 27-29.
[0186] The rotation position of the switching valve 80a is
controlled to change from the first rotation position to the second
rotation position, or from the second rotation position to the
first rotation position according to a flowchart of FIG. 27.
[0187] First, at step 250, it is judged if it is the time for
changing the rotation position of the switching valve 80a. The time
is, for example, each time a constant period has elapsed, or a time
when the total amount of the particulates flowing into the
particulate filter 22 reaches a certain constant amount, or a time
when the engine is decelerated.
[0188] At step 250, when it is judged that it is the time for
changing the rotation position of the switching valve 80a, the
routine proceeds to step 251 where the rotation position of the
switching valve 80a is changed.
[0189] On the other hand, at step 250, when it is judged that it is
not time for changing the rotation position of the switching valve
80a, the routine proceeds to step 252 without changing the rotation
position of the switching valve 80a.
[0190] At step 252, it is judged if the amount of the particulates
Apm flowing into the particulate filter 22 (hereinafter, referred
to as inflowing particulate amount) exceeds a predetermined amount
ApmTH (Apm>ApmTH). The inflowing particulate amount is
calculated using an integration of the emitted particulate amounts,
or pressure loss produced by the particulate filter 22 if there is
a pressure loss between the upstream and downstream ends of the
particulate filter 22, or difference in the particulate amount
removable by oxidation and the emitted particulate amount, or an
output of a sensor arranged downstream of the particulate filter 22
for detecting the concentration of the particulate.
[0191] At step 252, when it is judged that Apm>ApmTH, the
routine proceeds to step 253 where a temperature raising process is
performed for raising the temperature of the particulate filter 22
to the particulate oxidizing temperature to oxidize the deposited
particulates.
[0192] On the other hand, at step 252, when it is judged that
Apm.ltoreq.ApmTH, the routine proceeds to step 254 without
performing the temperature raising process.
[0193] At step 254, the process for preventing the thermal
deterioration is performed according to a flowchart of FIG. 28.
[0194] An explanation will be given of the process for preventing
the thermal deterioration, referring to FIG. 28. First, at step
300, it is judged if the temperature TF of the particulate filter
22 is higher than a predetermined temperature (For example,
particulate ignition temperature) TFTH (TF>TFTH).
[0195] At step 300, when it is judged that TF.ltoreq.TFTH, it is
considered that the particulate filter 22 will not be thermally
deteriorated. Then, the routine is ended.
[0196] On the other hand, at step 300, when it is judged that
TF>TFTH, the routine proceeds to step 301 where it is judged if
the present engine operation A is within the region D (A=D) on the
basis of a map of FIGS. 29A and 29B. In the map of FIGS. 29A and
29B, the region D is a dangerous region in which the particulate
filter 22 will be thermally deteriorated, and the region S is a
safety region in which the particulate filter 22 will not be
thermally deteriorated.
[0197] FIG. 29A shows a map used when the engine is operated under
a lean air-fuel ratio. According to the map of FIG. 29A, the
smaller the amount of the intake air, the smaller the amount of the
exhaust gas passing the particulate filter 22. Therefore, when the
amount of the heat radiated from the particulate filter 22 is
small, the possibility that the engine operation A is within the
dangerous region D is high.
[0198] Further, the larger the concentration Co of the oxygen in
the exhaust gas, the larger the amount of the oxygen flowing into
the particulate filter 22. Therefore, when the concentration Co of
the oxygen in the exhaust gas is large, the possibility that the
engine operation A is within the dangerous region D is high.
[0199] A line Lds for separating the dangerous region D from the
safety region S moves toward the safety region S when the
concentration Chc of the hydrocarbon (HC) in the exhaust gas
becomes large. That is, the possibility that the thermal
deterioration occurs becomes large when the concentration Chc of HC
in the exhaust gas becomes large.
[0200] On the other hand, FIG. 29B shows a map used when the engine
is operated under a lean air-fuel ratio close to the stoichiometric
air-fuel ratio, or generally under the stoichiometric air-fuel
ratio, or under a rich air-fuel ratio.
[0201] According to the map of FIG. 29B, the smaller the amount of
the intake air, the larger the possibility that the engine
operation A is within the dangerous region D.
[0202] Further, the larger the concentration Co of the oxygen in
the exhaust gas, the larger the possibility that the engine
operation A is within the dangerous region D.
[0203] A line Lds for separating the dangerous region D from the
safety region A moves toward the dangerous region D when the
concentration Chc of HC in the exhaust gas becomes large. That is,
the possibility that the thermal deterioration occurs becomes large
when the concentration Chc of HC in the exhaust gas becomes
small.
[0204] The reason that the tendency of the change of the
possibility of the thermal deterioration according to the change of
the concentration of HC in the exhaust gas depends on the air-fuel
ratio is as follows.
[0205] When the engine is operated under the lean air-fuel ratio,
the concentration of the oxygen in the exhaust gas is large.
Therefore, even if the concentration of HC in the exhaust gas
becomes large and, thus, the oxygen in the exhaust gas reacts with
HC and is consumed, the amount of the oxygen remaining in the
exhaust gas is sufficient for burning the deposited particulates in
the particulate filter 22 for short time.
[0206] Further, if the concentration of HC in the exhaust gas
becomes large, the amount of HC reacting with the oxygen becomes
large. Therefore, the temperature of the particulate filter 22 is
largely raised by the reaction of HC with the oxygen, so the
possibility of the thermal deterioration becomes large.
[0207] On the other hand, when the engine is operated under the
lean air-fuel ratio close to the stoichiometric air-fuel ratio, or
under the stoichiometric air-fuel ratio, or the rich air-fuel
ratio, the amount of the oxygen in the exhaust gas is originally
small. Therefore, when the concentration of HC in the exhaust gas
becomes large, and thus HC in the exhaust gas reacts with the
oxygen, the amount of the oxygen remaining in the exhaust gas is
insufficient for burning the deposited particulates all at once, so
the possibility of the thermal deterioration becomes small opposite
to the case that the engine is operated under the lean air-fuel
ratio.
[0208] At step 301, when it is judged that A=D, it is considered
that the particulate filter 22 will be thermally deteriorated, the
routine proceeds to step 302 where a switching valve control is
performed to make the rotation position of the switching valve at
neutral position, and then the routine proceeds to step 303.
[0209] At step 303, it is judged if the engine operation A is
within the safety region S (A=S). At step 303, when it is judged
that A=S, the routine proceeds to step 304. On the other hand, at
step 303, when it is judged that A.apprxeq.S, that is, AD, step 303
continues to be performed until, at step 303, it is judged that
A=S. Therefore, after the rotation position of the switching valve
80a is positioned at the neutral position at step 302, the rotation
position of the switching valve 80a is fixed at the neutral
position until it is judged that A=S at step 303.
[0210] At step 301, if it is judged that A.apprxeq.D, that is, A=S,
it is considered that the particulate filter 22 will not be
thermally deteriorated, and then the routine proceeds to step
304.
[0211] It may be considered that the particulate filter 22 will not
be thermally deteriorated even if the routine is ended to perform
the switching valve control shown in FIG. 27 when it is judged that
A=S at step 303 and thus the particulate filter 22 will not be
thermally deteriorated. However, in this flowchart, steps following
step 304 are added to assuredly prevent the thermal deterioration
of the particulate filter 22.
[0212] That is, the temperature TF of the particulate filter 22 is
still higher than the predetermined temperature TFTH even when it
is judged that the engine operation A is within the safety region S
at step 303. Further, the temperature TF of the particulate filter
22 may be locally high even when the temperature TF of the
particulate filter 22 is lower than the predetermined temperature
TFTH.
[0213] Under these condition, if the routine of FIG. 28 is ended,
and the rotation position of the switching valve 80a is changed
between the first and second rotation positions, the inflowing
direction of the exhaust gas is repeatedly inverted by changing the
rotation position of the switching valve 80a, so the heat is
concentrated on the central portion of the particulate filter 22,
and then the deposited particulates may burn all at once.
[0214] In this embodiment, to avoid the burning of the deposited
particulates all at once, a safety degree which indicates the
possibility that the particulate filter 22 will not be thermally
deteriorated is evaluated on the basis of the temperature and
amount of the exhaust gas, and the amounts of the oxygen and HC
flowing into the particulate filter 22 and, then, only when the
safety degree becomes large, is the routine of FIG. 28 ended and
the routine returns to that of FIG. 27.
[0215] To this end, at step 303, when it is judged that A=S and
thus the particulate filter 22 will not be thermally deteriorated,
the routine proceeds to step 304 where the rotation position of the
switching valve 80a is positioned at the first or second rotation
position, and then the routine proceeds to step 305.
[0216] At step 305, it is judged if the safety counter CS, which is
calculated according to a flowchart of FIG. 30, is larger than a
predetermined value CSTH (CS>CSTH).
[0217] According to the flowchart of FIG. 30, first, at step 400,
it is judged if the temperature Tex of the exhaust gas flowing into
the particulate filter 22 is lower than a predetermined temperature
TexTH (Tex<TexTH).
[0218] At step 400, when it is judged that Tex<TexTH, the
routine proceeds to step 401 where the safety counter CS is counted
up, and then proceeds to step 402. On the other hand, at step 400,
when it is judged that Tex.gtoreq.TexTH, the routine directly
proceeds to step 402.
[0219] At step 402, it is judged if the amount Gex of the exhaust
gas flowing into the particulate filter 22 is larger than a
predetermined amount Gex (Gex>GexTH).
[0220] At step 402, when it is judged that Gex>GexTH, the
routine proceeds to step 403 where the safety counter CS is counted
up, and then proceeds to step 404. On the other hand, when it is
judged that Gex.ltoreq.GexTH, the routine directly proceeds to step
404.
[0221] At step 404, it is judged if the amount Co of the oxygen in
the exhaust gas flowing into the particulate filter 22 is smaller
than a predetermined amount CoTH (Co<CoTH).
[0222] At step 404, when it is judged that Co<CoTH, the routine
proceeds to step 405 where the safety counter CS is counted up, and
then proceeds to step 406. On the other hand, at step 404, when it
is judged that Co.gtoreq.CoTH, the routine directly proceeds to
step 406.
[0223] At step 406, it is judged if the concentration Chc of HC in
the exhaust gas flowing into the particulate filter 22 is smaller
than a predetermined concentration ChcTH (Chc<ChcTH). At step
406, when it is judged that Chc<ChcTH, the routine proceeds to
step 407 where the safety counter CS is counted up and then is
ended. On the other hand, at step 406, when it is judged that
Chc.gtoreq.ChcTH, the routine is ended.
[0224] At step 305 of FIG. 28, when it is judged that CS>CSTH on
the basis of the safety counter CS calculated as explained above,
it is considered that the possibility that the deposited
particulates burn all at once is almost zero, and the routine
proceeds to step 306 where the safety counter CS is reset, and then
is ended.
[0225] On the other hand, at step 305, when it is judged that
CS.ltoreq.CSTH, it is considered that the deposited particulates
will burn all at once, and the routine returns to step 301. That
is, under the condition that the deposited particulates can burn
all at once, the engine operation A may enter into the dangerous
region D, so the routine returns to step 301 to assuredly prevent
the thermal deterioration of the particulate filter 22 even when
the engine operation A enters into the dangerous region D.
[0226] In the above explained process for preventing the thermal
deterioration, at step 304, after the rotation position of the
switching valve 80a is positioned at the first or second rotation
position, the rotation position of the switching valve 80a is fixed
until the safety degree becomes larger than a certain threshold
under the present engine operation.
[0227] However, an injector arranged in the exhaust pipe may inject
water or nitrogen to the particulate filter 22 to force the
temperature of the particulate filter 22 lower, thereby making the
safety degree larger than the certain threshold. Alternatively,
using only the temperature of the particulate filter 22 instead of
the safety degree, when the temperature TF of the particulate
filter 22 becomes lower than the predetermined temperature TFTH, or
lower than a temperature lower than the predetermined temperature
TFTH, the routine may return to the flowchart of FIG. 27.
[0228] Next, an explanation will be given of a process for
preventing the thermal deterioration of the second embodiment of
the invention. In this embodiment, immediately after it is judged
that the engine operation is within the dangerous region, the
exhaust gas is made not to bypass the particulate filter.
[0229] In this embodiment, it is judged if the engine operation
will move into the safety region within a range permitted in
consideration of several matters such as cost of fuel or required
engine load when the engine operating condition is changed. When it
is judged that the engine operation will move into the safety
region within the permitted range, the engine operating condition
is changed to move the engine operation into the safety region.
[0230] The parameters for determining if the engine operation is
within the safety region or the dangerous region are the
temperature of the particulate filter 22, the concentration of the
oxygen in the exhaust gas, the amount of the intake air, and the
concentration of HC in the exhaust gas.
[0231] Therefore, in order to move the engine operation into the
safety region, when the engine is operated under a relatively large
air-fuel ratio, the temperature of the particulate filter 22 is
lowered, or the concentration of the oxygen in the exhaust gas is
reduced, or the amount of the intake air is increased, or the
concentration of HC in the exhaust gas is reduced. Further, when
the engine is operated under a relatively small air-fuel ratio, the
concentration of HC in the exhaust gas is increased.
[0232] In order to lower the temperature of the particulate filter
22, for example, the pressure of the injection of the fuel from the
fuel injector is increased and the timing thereof is delayed.
[0233] In order to increase the amount of the intake air, for
example, the EGR rate is reduced, or if necessary, the EGR rate is
reduced to zero, or the transmission gear ratio is increased
compared with the present ratio to increase the engine speed if the
engine comprises an automatic gear ratio transmission.
[0234] When the EGR rate is reduced to zero, the speed of the fuel
combustion in the combustion chamber 5 becomes very fast, and thus
the level of the noise derived from the fuel combustion may become
larger than a permitted level, so it is preferable that a pilot
injection is performed for preliminarily injecting a small amount
of fuel before fuel is injected into the combustion chamber 5, or
that the pressure of the fuel injection is reduced to suppress the
increase of the level of the noise derived from the fuel
combustion.
[0235] In order to reduce the concentration of the oxygen in the
exhaust gas, the air-fuel ratio is reduced, or the EGR rate is
increased.
[0236] It is preferable that the air-fuel ratio is reduced when the
engine is operated under a relatively small air-fuel ratio, such as
when the low temperature combustion is performed, or when fuel
injection is performed at the combustion stroke other than the fuel
injection to inject fuel for operating the engine.
[0237] In this way, it is possible to avoid that the exhaust gas
including particulate directly discharges to the outside air
without passing the particulate filter 22 when the engine operating
condition is changed. When the engine operation does not enter into
the safety region even if the engine operating condition is
changed, a process similar to the process for preventing the
thermal deterioration of the first embodiment is performed so that
the exhaust gas is made to bypass the particulate filter 22.
[0238] FIG. 31 shows a flowchart for performing the process for
preventing the thermal deterioration of the second embodiment. In
the flowchart shown in FIG. 31, steps 500-506 except for steps 501a
and 501b correspond to steps 300-306 of FIG. 28.
[0239] In the flowchart shown in FIG. 31, at step 501, when it is
judged that the engine operation A is within the dangerous region D
(A=D), the routine proceeds to step 501a where it is judged if the
engine operation A will move into the safety region S by changing
the engine operating condition.
[0240] At step 501a, when it is judged that engine operation A will
move into the safety region S, the routine proceeds to step 501b
where the engine operating condition is changed so that the engine
operation A enters into the safety region S.
[0241] On the other hand, at step 501a, when it is judged that
engine operation A will not be able to move into the safety region
S, the routine proceeds to step 502. The remaining steps are the
same as those of FIG. 31, so explanations thereof are
eliminated.
[0242] When the amount of the exhaust gas flowing into the
particulate filter 22 should be reduced, in order to burn the
deposited particulates in the particulate filter 22 gradually and
not all at once, the bypass mechanism shown in FIGS. 22-25 may be
used to pass a small amount of exhaust gas into the particulate
filter 22.
[0243] In this case, the rotation position of the switching valve
80 is positioned at a position slightly displaced from the neutral
position toward the first or second rotation position. In this way,
a difference in pressures at the first and second ends of the
particulate filter 22 occurs, so a small amount of the exhaust gas
flows into the particulate filter 22.
[0244] Next, an explanation will be given of a process for removing
the deposited particulates by oxidation of the third embodiment,
including preventing the thermal deterioration of the particulate
filter, by referring to FIG. 32. The process for preventing the
thermal deterioration of the particulate filter of this embodiment
uses several concepts used in the first and second embodiments, and
further includes a process for removing SO.sub.x from the
particulate filter.
[0245] In a flowchart shown in FIG. 32, first, at step 600, it is
judged if the amount of the deposited particulates Apm is larger
than a predetermined amount ApmTH (Apm>ApmTH). The amount of the
deposited particulates Apm is, for example, calculated by
integrating an amount of the deposited particulates per unit time
which is previously obtained by an experiment as a function of the
engine speed N and the required engine load L.
[0246] At step 600, when it is judged that Apm>ApmTH, that is,
it is judged that the deposited particulates should be removed by
oxidation, the routine proceeds to step 601 where a temperature
raising process is performed for raising the temperature of the
particulate filter 22 to the particulate oxidable temperature, and
then proceeds to step 602.
[0247] For example, in order to raise the temperature of the
particulate filter, the low temperature combustion is performed.
Alternatively, in order to raise the temperature of the particulate
filter, an exhaust throttle valve arranged in the exhaust passage
may be closed to increase the required engine load, thus increasing
the amount of the injected fuel.
[0248] Further, in order to raise the temperature of the
particulate filter, a small amount of the fuel may be injected
during the combustion stroke other than the fuel for operating the
engine, and burned to raise the temperature of the exhaust gas.
[0249] On the other hand, at step 600, it is judged that Apm
.ltoreq.ApmTH, the routine directly proceeds to step 602.
[0250] At step 602, a process for preventing the thermal
deterioration is performed according to a flowchart shown in FIG.
33. In the flowchart shown in FIG. 33, first, at step 605, it is
judged if a condition (thermal deterioration preventing condition),
that the process for preventing the thermal deterioration should be
performed, is satisfied. Further, this is judged according to a
flowchart shown in FIG. 34.
[0251] In the flowchart shown in FIG. 34, first, at step 700, it is
judged if the temperature TF of the particulate filter 22 is higher
than a predetermined temperature TFTH (TF>TFTH). The
predetermined temperature is, for example, set at the particulate
ignition temperature.
[0252] At step 700, when it is judged that TF>TFTH, the routine
proceeds to step 701 where it is judged that the thermal
deterioration preventing condition is satisfied.
[0253] On the other hand, at step 700, when it is judged that
TF.ltoreq.TFTH, it is judged that the thermal deterioration
preventing condition is not satisfied, and then the routine is
ended.
[0254] At step 605 of FIG. 33, when the thermal deterioration
preventing condition is satisfied, the routine proceeds to step 606
where the process for preventing the thermal deterioration is
performed.
[0255] In the process for preventing the thermal deterioration, the
exhaust gas is made to bypass the particulate filter 22 to make the
amount of the exhaust gas flowing into the particulate filter 22
lower than a first threshold, preferably generally zero, or the
amount of the intake air is reduced to make the amount of the
exhaust gas flowing into the particulate filter 22 lower than a
first threshold, or the engine speed is increased to make the
amount of the exhaust gas flowing into the particulate filter 22
larger than a second threshold.
[0256] The first threshold is the amount of the exhaust gas which
is small sufficient for suppressing the burning of the deposited
particulates. The second threshold is the amount of the exhaust gas
which is large enough to radiating the heat of the burning of the
deposited particulates to prevent the thermal deterioration of the
particulate filter 22.
[0257] The process for preventing the thermal deterioration is
stopped after a predetermined period has elapsed, and then the
normal process starts to be performed. The predetermined period is,
for example, a period sufficient for lowering the temperature of
the particulate filter 22 to near the particulate oxidizing
temperature.
[0258] At step 603 of FIG. 32, it is judged if the amount As of the
sulfur S adhered to the particulate filter 22 is larger than a
predetermined amount AsTH (As>AsTH).
[0259] The sulfur S contained in the exhaust gas adheres to the
surface of the particulate filter 22. When the particulate filter
22 comprises NO.sub.x absorbent having NO.sub.x absorbing and
discharging capacity which absorbs and holds NO.sub.x when the
oxygen is excessive in the surroundings, and discharges the held
NO.sub.x when the concentration of the oxygen in the surroundings
lowers, the adhering sulfur suppresses the NO.sub.x absorbing and
discharging capacity.
[0260] Therefore, in this flowchart, at step 603, when it is judged
that the amount of the adhering sulfur S is relatively large, a
process is performed for removing the adhering sulfur S from the
particulate filter 22.
[0261] Note that the active oxygen release agent is used with the
precious metal catalyst such as platinum Pt. Further, as the active
oxygen release agent, use is made of at least one of an alkali
metal such as potassium K, sodium Na, lithium Li, cesium Cs, and
rubidium Rb, an alkali earth metal such as barium Ba, calcium Ca,
and strontium Sr, a rare earth such as lanthanum La, yttrium Y, and
cerium Ce, a transition metal such as iron Fe, and a carbon family
element such as tin Sn.
[0262] In detail, at step 603, it is judged that As>AsTH, the
routine proceeds to step 604 where the engine is operated under the
rich air-fuel ratio to make the air-fuel ratio of the exhaust gas
richer than the stoichiometric air-fuel ratio. Thereby, the
concentration of the oxygen in the particulate filter 22 is reduced
while the hydrocarbon in the exhaust gas reacts with the oxygen to
raise the temperature of the particulate filter 22. Therefore, the
sulfur S adhering to the particulate filter 22 is disassociated
from the particulate filter 22.
[0263] The temperature for disassociating the sulfur from the
particulate filter 22 is higher than the particulate oxidizing
temperature, so it is preferable, in view of energy efficiency,
that the temperature of the particulate filter 22 is raised to the
sulfur disassociating temperature after the temperature of the
particulate filter 22 is raised to the particulate oxidizing
temperature at step 601.
[0264] As explained above, in this embodiment, when the amount of
deposited particulates is larger than the predetermined amount, the
temperature raising process is performed. Alternatively, the
temperature raising process may be performed when the difference in
the pressures (pressure loss) of the exhaust gas upstream and
downstream of the particulate filter 22 is larger than a
predetermined level if the pressure loss occurs.
[0265] Further, as explained above, in this embodiment, it is
judged if the thermal deterioration preventing process should be
performed on the basis of the temperature of the particulate filter
22. Alternatively, in addition to the temperature of the
particulate filter 22, the amount of the intake air flowing into
the combustion chamber, or the amount of the exhaust gas flowing
into the particulate filter 22 (inflowing exhaust gas amount) may
be used to judge if the thermal deterioration preventing process
should be performed.
[0266] FIG. 35 shows a flowchart of another embodiment for judging
if the thermal deterioration preventing condition is satisfied on
the basis of the temperature TF of the particulate filter 22 and
the inflowing exhaust gas amount Gex.
[0267] In the flowchart shown in FIG. 35, first, at step 800, it is
judged if the temperature TF of the particulate filter 22 is higher
than the predetermined temperature TFTH (TF>TFTH).
[0268] At step 800, when it is judged that TF>TFTH, the routine
proceeds to step 801 where it is judged if the inflowing exhaust
gas amount Gex is larger than a minimum amount GexMin and is
smaller than a maximum amount GexMax (GexMin<Gex<GexMax).
[0269] At step 801, when it is judged that GexMin<Gex<Gexmax,
that is, when it is judged that the temperature of the particulate
filter 22 is higher than the particulate ignition temperature, and
the inflowing exhaust gas amount is insufficient for rapidly
radiating the heat of the burning of the deposited particulates,
and the inflowing oxygen amount is sufficient for promoting the
burning of the deposited particulates, it is considered that the
thermal deterioration of the particulate filter 22 should be
prevented, so the routine proceeds to step 802 where it is judged
that the thermal deterioration preventing condition is
satisfied.
[0270] Note that the present invention can also be applied to an
exhaust gas purification apparatus designed to arrange an oxidation
catalyst in the exhaust passage upstream of the particulate filter,
convert the NO in the exhaust gas to NO.sub.2 by this oxidation
catalyst, cause the NO.sub.2 and the particulates deposited on the
particulate filter to react, and use this NO.sub.2 to oxidize the
particulates.
[0271] According to the present invention, as explained above, it
is possible to continuously oxidize and remove the particulates in
the exhaust gas on the particulate filter while purifying the
NO.sub.x in the exhaust gas well.
[0272] While the invention has been described with reference to
specific embodiments chosen for purpose of illustration, it should
be apparent that numerous modifications could be made thereto by
those skilled in the art without departing from the basic concept
and scope of the invention.
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